Nonlinear Fokker Planck Equations

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Springer Complexity Springer Complexity is a publication program, cutting across all traditional disciplines of sciences as well as engineering, economics, medicine, psychology and computer sciences, which is aimed at researchers, students and practitioners working in the field of complex systems. Complex Systems are systems that comprise many interacting parts with the ability to generate a new quality of macroscopic collective behavior through self-organization, e.g., the spontaneous formation of temporal, spatial or functional structures. This recognition, that the collective behavior of the whole system cannot be simply inferred from the understanding of the behavior of the individual components, has led to various new concepts and sophisticated tools of complexity. The main concepts and tools – with sometimes overlapping contents and methodologies – are the theories of self-organization, complex systems, synergetics, dynamical systems, turbulence, catastrophes, instabilities, nonlinearity, stochastic processes, chaos, neural networks, cellular automata, adaptive systems, and genetic algorithms. The topics treated within Springer Complexity are as diverse as lasers or fluids in physics, machine cutting phenomena of workpieces or electric circuits with feedback in engineering, growth of crystals or pattern formation in chemistry, morphogenesis in biology, brain function in neurology, behavior of stock exchange rates in economics, or the formation of public opinion in sociology. All these seemingly quite different kinds of structure formation have a number of important features and underlying structures in common. These deep structural similarities can be exploited to transfer analytical methods and understanding from one field to another. The Springer Complexity program therefore seeks to foster crossfertilization between the disciplines and a dialogue between theoreticians and experimentalists for a deeper understanding of the general structure and behavior of complex systems. The program consists of individual books, books series such as “Springer Series in Synergetics", “Institute of Nonlinear Science", “Physics of Neural Networks", and “Understanding Complex Systems", as well as various journals.

Springer Series in Synergetics Series Editor Hermann Haken Institut für Theoretische Physik und Synergetik der Universität Stuttgart 70550 Stuttgart, Germany and Center for Complex Systems Florida Atlantic University Boca Raton, FL 33431, USA

Members of the Editorial Board Åke Andersson, Stockholm, Sweden Gerhard Ertl, Berlin, Germany Bernold Fiedler, Berlin, Germany Yoshiki Kuramoto, Sapporo, Japan Jürgen Kurths, Potsdam, Germany Luigi Lugiato, Milan, Italy Jürgen Parisi, Oldenburg, Germany Peter Schuster, Wien, Austria Frank Schweitzer, Zürich, Switzerland Didier Sornette, Los Angeles, CA, USA, and Nice, France Manuel G. Velarde, Madrid, Spain SSSyn – An Interdisciplinary Series on Complex Systems The success of the Springer Series in Synergetics has been made possible by the contributions of outstanding authors who presented their quite often pioneering results to the science community well beyond the borders of a special discipline. Indeed, interdisciplinarity is one of the main features of this series. But interdisciplinarity is not enough: The main goal is the search for common features of self-organizing systems in a great variety of seemingly quite different systems, or, still more precisely speaking, the search for general principles underlying the spontaneous formation of spatial, temporal or functional structures. The topics treated may be as diverse as lasers and fluids in physics, pattern formation in chemistry, morphogenesis in biology, brain functions in neurology or self-organization in a city. As is witnessed by several volumes, great attention is being paid to the pivotal interplay between deterministic and stochastic processes, as well as to the dialogue between theoreticians and experimentalists. All this has contributed to a remarkable cross-fertilization between disciplines and to a deeper understanding of complex systems. The timeliness and potential of such an approach are also mirrored – among other indicators – by numerous interdisciplinary workshops and conferences all over the world.

Till Daniel Frank

Nonlinear Fokker–Planck Equations Fundamentals and Applications

With 86 Figures and 18 Tables

123

Dr. Till Daniel Frank Universität Münster Institut für Theoretische Physik Wilhelm-Klemm-Strasse 9 48149 Münster, Germany

ISSN 0172-7389 ISBN 3-540-21264-7 Springer Berlin Heidelberg New York This work is subject to copyright. All rights are reserved, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilm or in any other way, and storage in data banks. Duplication of this publication or parts thereof is permitted only under the provisions of the German Copyright Law of September 9, 1965, in its current version, and permission for use must always be obtained from Springer. Violations are liable to prosecution under the German Copyright Law. Springer is a part of Springer Science+Business Media springeronline.com © Springer-Verlag Berlin Heidelberg 2005 Printed in Germany The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Typesetting: by the author Cover design: design & production, Heidelberg Printed on acid-free paper 55/3141/ts 543210

This book is dedicated to my parents, wife and daughter.

Preface

Nonlinear Fokker–Planck equations have found applications in various fields such as plasma physics, surface physics, astrophysics, the physics of polymer fluids and particle beams, nonlinear hydrodynamics, theory of electronic circuitry and laser arrays, engineering, biophysics, population dynamics, human movement sciences, neurophysics, psychology and marketing. In spite of the diversity of these research fields, many phenomena addressed therein have a fundamental physical mechanism in common. They arise due to cooperative interactions between the subsystems of many-body systems. These cooperative interactions result in a reduction of the large number of degrees of freedom of many-body systems and, in doing so, bind the subunits of manybody systems by means of self-organization into synergetic entities. These synergetic many-body systems admit low dimensional descriptions in terms of nonlinear Fokker–Planck equations that capture and uncover the essential dynamics underlying the observed phenomena. The phenomena that will be addressed in this book range from equilibrium and nonequilibrium phase transitions and the multistability of systems to the emergence of power law and cut-off distributions and the distortion of Boltzmann distributions. We will study possible asymptotic behaviors of systems such as the approach to stationary distributions and the emergence of nonstationary traveling wave distributions. We will be concerned with normal and anomalous diffusion and we will examine how correlation functions evolve with time in these kinds of synergetic systems. We will discuss a Fokker–Planck approach to quantum statistics, linear nonequilibrium thermodynamics, and generalized extensive and nonextensive thermostatistics. The aim of this book is to provide an introduction to the theory of nonlinear Fokker–Planck equations and to highlight what systems described by nonlinear Fokker–Planck equations have in common. Theoretical considerations and concepts will be illustrated by various examples and applications. Due to the ramifications of the theory of nonlinear Fokker–Planck equations in various scientific fields, this book is designed for graduate students and researchers in physics and related fields such as biology, neurophysics, human movement sciences, and psychology. I hope that this book will make graduate students interested in the topic of nonlinear Fokker–Planck equa-

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Preface

tions and will make researchers aware of the connections between the different areas in which nonlinear Fokker–Planck equations have been applied so far. Acknowledgments I am indebted to Professor H. Haken for inviting me to write a book on the topic of nonlinear Fokker–Planck equations for the Springer Series of Synergetics. I am grateful to Professor P.J. Beek and Professor R. Friedrich for supporting my studies on nonlinear Fokker-Planck equations. I would like to thank Dr. A. Daffertshofer for many helpful discussions. Finally, I wish to thank Professor W. Beiglb¨ ock and Ms. B. Reichel-Mayer of the SpringerVerlag for their help in preparing this manuscript.

M¨ unster, September 2004

Till Daniel Frank

Contents

1

Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.1 Fokker–Planck Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.1.1 Brownian Particles and Langevin Equations . . . . . . . . . 1.1.2 Many-Body Systems and Mean Field Theory . . . . . . . . 1.2 Phase Transitions and Self-Organization . . . . . . . . . . . . . . . . . . . 1.3 Stochastic Feedback . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4 Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.1 Collective Phenomena . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.2 Multistable Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.3 Power Law and Cut-Off Distributions . . . . . . . . . . . . . . . 1.4.4 Free Energy Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.5 Anomalous Diffusion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.5 Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

1 1 1 2 3 5 7 7 7 10 12 15 16

2

Fundamentals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1 Stochastic Processes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2 Nonlinear Fokker–Planck Equation . . . . . . . . . . . . . . . . . . . . . . . 2.2.1 Notation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.2 Stratonovich Form . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.3 Transient Solutions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.4 Continuity Equation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.5 Boundary Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.6 Stationary Solutions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3 Self-Consistency Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4 Multistability and Basins of Attraction . . . . . . . . . . . . . . . . . . . . 2.5 Nonlinearity Dimension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6 Classifications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.7 Derivations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.8 Numerics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.8.1 Path Integral Solutions . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.8.2 Fourier and Moment Expansions . . . . . . . . . . . . . . . . . . . 2.8.3 Finite Difference Schemes . . . . . . . . . . . . . . . . . . . . . . . . . 2.8.4 Distributed Approximating Functionals . . . . . . . . . . . . .

19 19 20 21 21 22 22 23 23 24 25 25 26 28 28 28 29 29 30

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Contents

Strongly Nonlinear Fokker–Planck Equations . . . . . . . . . . . . . 3.1 Transformation to a Linear Problem . . . . . . . . . . . . . . . . . . . . . . 3.2 What Are Strongly Nonlinear Fokker–Planck Equations? . . . . 3.3 Correlation Functions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4 Langevin Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4.1 Two-Layered Langevin Equations . . . . . . . . . . . . . . . . . . 3.4.2 Self-Consistent Langevin Equations . . . . . . . . . . . . . . . . . 3.4.3 Hierarchies and Correlation Functions . . . . . . . . . . . . . . . 3.4.4 Numerics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.5 Stationary Solutions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.6 H-Theorem for Stochastic Processes . . . . . . . . . . . . . . . . . . . . . . . 3.7 Nonlinear Families of Markov Processes∗ . . . . . . . . . . . . . . . . . . 3.7.1 Linear Versus Nonlinear Families of Markov Processes 3.7.2 Linear Families of Markov Processes . . . . . . . . . . . . . . . . 3.7.3 Nonlinear Families of Markov Diffusion Processes . . . . . 3.7.4 Markov Embedding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.7.5 Hitchhiker Processes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.8 Top-Down Versus Bottom-Up Approaches∗ . . . . . . . . . . . . . . . . 3.9 Transient Solutions and Transition Probability Densities . . . . . 3.9.1 Nonequivalence of Transient Solutions and Transition Probability Densities . . . . . . . . . . . . . . . . 3.9.2 Gaussian Distributions∗ . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.9.3 Purely Random Processes . . . . . . . . . . . . . . . . . . . . . . . . . 3.9.4 Wiener Processes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.9.5 Ornstein–Uhlenbeck Processes . . . . . . . . . . . . . . . . . . . . . 3.9.6 Transient Solutions: Two Examples . . . . . . . . . . . . . . . . . 3.10 Shimizu–Yamada Model – Transient Solutions . . . . . . . . . . . . . . 3.11 Fluctuation–Dissipation Theorem . . . . . . . . . . . . . . . . . . . . . . . . .

31 31 33 36 36 36 38 39 39 42 43 46 46 47 48 50 50 52 55

Free Energy Fokker–Planck Equations . . . . . . . . . . . . . . . . . . . . 4.1 Free Energy Principle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.2 Maximum Entropy Principle and Relationship between Noise Amplitude and Temperature . . . . . . . . . . . . . . . . 4.3 H-Theorem for Free Energy Fokker–Planck Equations . . . . . . . 4.4 Boltzmann Statistics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.5 Linear Nonequilibrium Thermodynamics . . . . . . . . . . . . . . . . . . 4.5.1 Derivation of Free Energy Fokker–Planck Equations . . 4.5.2 Drift and Diffusion Coefficients . . . . . . . . . . . . . . . . . . . . . 4.5.3 Transition Probability Densities and Langevin Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.5.4 Density Functions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.5.5 Entropy Production and Conservative Force . . . . . . . . . 4.5.6 Stationary Solutions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.5.7 H-Theorem for Systems with Conservative Forces and Nontrivial Mobility Coefficients . . . . . . . . . . . . . . . .

73 75

55 57 61 62 62 63 66 70

76 77 79 80 80 84 86 87 87 88 89

Contents

4.6 Canonical-Dissipative Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.6.1 Linear Case . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.6.2 Nonlinear Case . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.7 Boundedness of Free Energy Functionals∗ . . . . . . . . . . . . . . . . . . 4.7.1 Distortion Functionals . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.7.2 Kullback Measure and Entropy Inequality . . . . . . . . . . . 4.7.3 Generic Cases and Schl¨ ogl’s Decomposition of Kullback Measures . . . 4.8 First, Second, and Third Choice Thermostatistics . . . . . . . . . . . 5

Free Energy Fokker–Planck Equations with Boltzmann Statistics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1 Stability Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1.1 Lyapunov’s Direct Method . . . . . . . . . . . . . . . . . . . . . . . . 5.1.2 Linear Stability Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1.3 Self-Consistency Equation Analysis . . . . . . . . . . . . . . . . . 5.1.4 Shiino’s Decomposition of Perturbations . . . . . . . . . . . . . 5.1.5 Generic Cases . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1.6 Higher-Dimensional Nonlinearities . . . . . . . . . . . . . . . . . . 5.1.7 Multiplicative Noise . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.1.8 Norm for Perturbations∗ . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2 Natural Boundary Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2.1 Shimizu–Yamada Model – Stationary Solutions . . . . . . 5.2.2 Dynamical Takatsuji Model – Basins of Attraction . . . . 5.2.3 Desai–Zwanzig Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2.4 Bounded B(M1 )-Model . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3 Periodic Boundary Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3.1 Cluster Amplitude and Cluster Phase . . . . . . . . . . . . . . . 5.3.2 KSS Model – Cluster Amplitude Dynamics . . . . . . . . . . 5.3.3 Mean Field HKB Model – Cluster Phase Dynamics . . . 5.4 Characteristics of Bifurcations . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.4.1 Stability and Disorder . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.4.2 Emergence of Collective Behavior . . . . . . . . . . . . . . . . . . 5.4.3 Multistability and Symmetry . . . . . . . . . . . . . . . . . . . . . . 5.4.4 Continuous and Discontinuous Phase Transitions . . . . . 5.5 Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.5.1 Ferromagnetism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.5.2 Synchronization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.5.3 Isotropic-nematic Phase Transitions and Maier–Saupe Model . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.5.4 Muscular Contraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.5.5 Network Models for Group Behavior . . . . . . . . . . . . . . . . 5.5.6 Multistable Perception-Action Systems . . . . . . . . . . . . . .

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90 90 92 96 97 97 100 107

109 110 112 113 115 118 120 126 130 132 134 135 140 148 152 155 156 157 167 183 183 184 186 187 188 188 191 195 202 206 209

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Entropy Fokker–Planck Equations . . . . . . . . . . . . . . . . . . . . . . . . 6.1 Existence and Uniqueness of Stationary Solutions∗ . . . . . . . . . . 6.2 Entropy Increase and Anomalous Diffusion . . . . . . . . . . . . . . . . 6.2.1 Entropy Increase . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.2.2 Anomalous Diffusion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.3 Drift- and Diffusion Forms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.4 Entropy and Information Measures . . . . . . . . . . . . . . . . . . . . . . . 6.4.1 Properties∗ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.4.2 Examples . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.5 Examples and Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.5.1 Porous Medium Equation . . . . . . . . . . . . . . . . . . . . . . . . . 6.5.2 TSq -Entropy Fokker–Planck Equation . . . . . . . . . . . . . . . 6.5.3 Sharma–Mittal Entropy Fokker–Planck Equation . . . . . 6.5.4 Fokker–Planck Equations for Fermions and Bosons . . . 6.5.5 Multivariate Generalizations . . . . . . . . . . . . . . . . . . . . . . . 6.5.6 Metal Electron Model, Black Body Radiation Model, and Planck’s Radiation Formula . . . . . . . . . . . . . . . . . . . . 6.5.7 Population Dynamics . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

213 215 218 218 219 222 224 224 231 246 246 250 261 280 284

7

General Nonlinear Fokker–Planck Equations . . . . . . . . . . . . . . 7.1 Linear Stability Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.1.1 Stationary Solutions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.1.2 Stability of Stationary Solutions . . . . . . . . . . . . . . . . . . . . 7.1.3 On an Additional Stability Coefficient∗ . . . . . . . . . . . . . . 7.2 Free Energy and Lyapunov Functional Analysis . . . . . . . . . . . . 7.2.1 Moving Frame Transformations . . . . . . . . . . . . . . . . . . . . 7.2.2 Derivation of Entropy and Information Measures . . . . . 7.2.3 Derivation of Local Lyapunov Functionals . . . . . . . . . . . 7.2.4 Derivation of Lyapunov Functionals . . . . . . . . . . . . . . . . . 7.3 Examples . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.3.1 Traveling Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.3.2 Reentrant Noise-Induced Phase Transitions . . . . . . . . . . 7.3.3 Systems with Multistable Variability . . . . . . . . . . . . . . . . 7.4 Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.4.1 Landau Form and Plasma Particles . . . . . . . . . . . . . . . . . 7.4.2 Bunch-Particle Distributions of Particle Beams . . . . . . . 7.4.3 Noise Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.4.4 Accuracy-Flexibility Trade-Off . . . . . . . . . . . . . . . . . . . . . 7.5 Bibliographic Notes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

299 299 299 300 305 306 306 310 312 317 324 324 329 332 341 341 342 349 351 360

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Epilogue . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 367

288 296

References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 371 Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 401

1 Introduction

1.1 Fokker–Planck Equations Fokker–Planck equations describe the evolution of stochastic systems. For example, they describe the erratic motions of small particles that are immersed in fluids, fluctuations of the intensity of laser light, velocity distributions of fluid particles in turbulent flows, and the stochastic behavior of exchange rates. In general, Fokker–Planck equations can be applied to equilibrium and nonequilibrium systems. That is, they can be applied to systems that operate close to stationary states of thermal equilibrium [89, 490, 576] and to systems that operate far from thermal equilibrium [263]. 1.1.1 Brownian Particles and Langevin Equations Let us consider a single particle – a so-called Brownian particle – that is in contact with its environment [282, 346, 490, 619]. In general, there are interactions between a Brownian particle and its environment. That is, the environment acts on the particle and the particle acts on the environment. A helpful notion of an environment is a heat bath composed of a large number of heat bath particles. From this point of view, a complete description of the systems at hand requires taking the state variables of the Brownian particle and the state variables of all heat bath particles into account. In many cases, however, a reduced description can be obtained that involves only the state variables of the Brownian particle. The interactions between the heat bath particles and the Brownian particle then result in two forces that act on the Brownian particle: a damping force and a fluctuating force [89, 254, 308, 317, 517]. For example, let X(t) denote the state variable of the Brownian particle. Then, the evolution of the Brownian particle may be given by d X(t) = −γX(t) + QΓ (t) , dt

(1.1)

where −γX is a linear damping force and γ is a positive damping constant. The function Γ (t) describes a fluctuating force which is only defined in √ a statistical sense. Q describes the strength of the fluctuating force. Since QΓ (t) describes the impact of a noise source on the Brownian particle, we also say that Q corresponds to a noise amplitude.

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1 Introduction

If Γ (t) in (1.1) describes a particular fluctuating force, namely, a Langevin force [221, 254, 498], then (1.1) is referred to as Langevin equation. For stochastic processes described by Langevin equations we can write evolution equations for the corresponding probability densities [221, 254, 498]. For example, for the stochastic process given by (1.1) the evolution equation of the probability density P reads ∂2 ∂ ∂ P (x, t) = γ xP (x, t) + Q 2 P (x, t) . ∂t ∂x ∂x

(1.2)

Equation (1.2) is an example of a linear Fokker–Planck equation. Stochastic processes described by linear Fokker–Planck equations such as (1.2) are called Markov diffusion processes [221, 298]. 1.1.2 Many-Body Systems and Mean Field Theory Many-body systems such as solids, neural networks, and social societies are composed of many interacting subsystems. A complete description of manybody systems requires taking the interactions between all subsystems into account. Often, many-body systems can approximately be described in terms of the evolution of a single subsystem or a few subsystems. Let us consider many-body systems that are composed of a single type of subsystem. Then, we may describe the interactions between a single subsystem and its fellow-subsystems by the force that on the average is exerted by all fellowsubsystems on the single subsystem. This force is called a mean field force and is described by means of a statistical measure. In order to obtain selfconsistent and closed single subsystem descriptions, one can express the averaging over the subsystems in terms of an averaging with respect to the statistical properties of the single subsystem under consideration [89]. Some systems to which this mean field treatment has been applied are listed in Table 1.1. Table 1.1. Applications of mean field theory Phenomenon

Theory

Ref.

Ferromagnetism Polarization Nematic phases Astrophysics

Weiss mean field theory Debye theory Maier–Saupe theory Vlasov approach

[57, 89, 229, 490, 546] [268, 319, 410] [90, 129, 458, 485, 551] [58, 92, 349, 527, 615]

In quantum mechanics, many-body systems can be treated in a similar manner. Here, using the Hartree–Fock theory, Schr¨ odiner equations for

1.2 Phase Transitions and Self-Organization

3

many-body problems can be reduced to single particle Schr¨ odinger equations. The single particle Schr¨ odinger equations, however, involve energy terms that depend on the statistical properties of the single particles that they describe [233, 269, 279, 502]. Furthermore, a mean field approach to the Bose-Einstein condensation has been developed that is centered around the Gross–Pitaevskii equation. The Gross–Pitaevskii equation is a single particle Schr¨ odinger equation that involves a probability-dependent coefficient and describes the behavior of a many-body system: a gas composed of Bose particles [78, 121, 137, 244, 478]. The one thing that all mean field theories have in common is that they yield nonlinear descriptions for single subsystems. The nonlinearities that occur in the single subsystem descriptions reflect the interactions between the subsystems of the many-body systems. The advantage of mean field models is that, on the one hand, they often can be solved with relatively little effort and, on the other hand, they account for subsystem-subsystem interactions of many-body systems. In line with mean field theory, one may describe many-body systems in terms of Fokker–Planck equations for single subsystem probability densities P (x, t). In order to account for subsystem-subsystem interactions, one may consider Fokker–Planck equations with probability-dependent coefficients that read like ∂ ∂2 ∂ P (x, t) = − Di (x, t, P )P (x, t) + Dik (x, t, P )P (x, t) . ∂t ∂xi ∂xi ∂xk i i,k

(1.3) We refer to (1.3) as a nonlinear Fokker–Planck equation. The distribution function P (x, t) has two faces. According to the µ-space description of manybody systems [97, 291, 437] (or the Maxwell-Boltzmann picture of many-body systems [490, 619]), we interpret P (x, t) as a function that describes the probability to find subsystems of a many-body system at time t in states x. In particular, if ρ(x, t) describes the mass density (or particle density) of a system with a total mass (or total particle number) M0 , then P is given by P = ρ/M0 . In line with mean field theory, P (x, t) is regarded as probability density of a single subsystem. In sum, P (x, t) describes the distribution of subsystems in the µ-space as well as the stochastic properties of single subsystems. This is because if mean field theory applies, then the stochastic properties of a single subsystem reflect the way the entire ensemble of subsystems is distributed.

1.2 Phase Transitions and Self-Organization There are numerous examples of equilibrium and nonequilibrium systems that exhibit transitions between phases and characteristic spatio-temporal

4

1 Introduction

patterns and behaviors. There are transitions between solid, fluid and gas phases of matter. Ferromagnets show transitions between phases with vanishing and non-vanishing magnetization. Lasers can produce ordinary light (i.e., ”chaotic” light) as well as laser light (i.e., coherent light) and show transitions between these qualitatively different regimes when their pumping energies are changed. Humans and animals change gaits at critical values of locomotion speeds. In human societies, there are transitions between fashion trends every now and then. In the following, we will refer to the phases of matter and the characteristic spatio-temporal manifestations of systems simply as phases. Transitions between phases will be referred to as (equilibrium and nonequilibrium) phase transitions. System parameters that are involved in phase transitions will be called control parameters. In order to quantify equilibrium and nonequilibrium phase transitions it is useful to describe systems by means of variables that capture the characteristic properties of phases: the order parameters. Phase transitions can then be described in terms of bifurcations of order parameters as illustrated in Fig. 1.1.

order parameter

0 0

critical value

control parameter

Fig. 1.1. Illustration of the bifurcation of an order parameter

The Landau theory of (second-order or continuous) phase transitions tells us that, in general, equilibrium systems at phase transition points exhibit order parameters [57, 229, 371, 372, 410, 546]. Moreover, the theory predicts that close to phase transition points the whole behavior of equilibrium systems can be described in terms of appropriately defined order parameters. That is, all quantities of interest can be expressed as functions of these order parameters. The order parameters of equilibrium systems typically correspond to mean field variables derived from mean field theory such as averaged magnetization. In a similar spirit, many nonequilibrium systems can be described in the vicinity of phase transition points by means of a few relevant variables [104,

1.3 Stochastic Feedback

5

365] and, in particular, by means of a few order parameters [55, 207, 211, 212, 252, 254, 255, 258, 260, 419, 444, 448, 486, 637]. As pointed out by Haken [254, 267, 270, 271], it is helpful to regard order parameters of nonequilibrium systems as counterparts to the order parameters of the Landau theory. What is the reason for the emergence of order parameters? Close to phase transition points, subsystems of many-body systems can evolve in a selforganized fashion. Due to self-organization, the degrees of freedom of manybody systems can be considerably reduced such that there are only a few degrees of freedom left. These remaining degrees of freedom then define low dimensional phase spaces in which order parameters evolve (see e.g. [254, 255]). Self-organizing systems described by nonlinear Fokker–Planck equations of the form (1.3) typically involve coefficients Di and Dik that depend on order parameters. For example, we may deal with a random variable X(t) described by a nonlinear Fokker–Planck equation ∂2 ∂ ∂ Di (x, t, m)P (x, t) + Dik (x, t, m)P (x, t) P (x, t) = − ∂t ∂xi ∂xi ∂xk i i,k

(1.4) that involves an order parameter m defined by m = X, where X is the average of X.

1.3 Stochastic Feedback In order to elucidate the notion of stochastic feedback we consider a field v(x, t) that describes the flow of a system. For example, v(x, t) may correspond to a component of a velocity vector field. We then assume that system variables ψi (x, t) change due to the flow of the system such that we obtain a linear transport equation ∂ ψi (x, t) = Fˆ (x, ∇, t, v) ψi (x, t) + Ri ∂t

(1.5)

involving an operator Fˆ (x, ∇, t, v) that depends on v and some source terms Ri . We say that the evolution of the field variables ψi (x, t) is determined by the flow field v(x, t). If v(x, t) satisfies (1.5) we deal with feedback. In this case (1.5) reads ∂ v(x, t) = Fˆ (x, ∇, t, v) v(x, t) + Rv ∂t

(1.6)

and is nonlinear with respect to v. Feedback of this kind can be found, for example, in hydrodynamics (hydrodynamic feedback). If we consider laminar flows in the direction of the x-coordinate, then v corresponds to the velocity

6

1 Introduction

field vx (x, t) of a fluid, Fˆ is given by Fˆ = −vx ∂/∂x, and the field variables ψi correspond to the density field of the fluid, the temperature field, and the velocity field vx (x, t) [448].

noise

many−body system X

conventional feedback

stochastic feedback ρ

Fig. 1.2. Basic features of a stochastic feedback system

Now let us interpret a probability density P as some kind of flow field v. Let us assume that the evolution of system variables ψi is affected by the flow field P (x, t) in such a way that we obtain the linear evolution equation (1.5) for v = P and Ri = 0: ∂ ψi (x, t) = Fˆ (x, ∇, t, P (x, t)) ψi (x, t) . ∂t

(1.7)

If P satisfies its own evolution equation, that is, for v = P (x, t), and if the operator Fˆ is given by Fˆ (x, ∇, t, P ) = −

∂ ∂2 Di (x, t, P ) + Dik (x, t, P ) , ∂xi ∂xi ∂xk i

(1.8)

i,k

then we obtain the nonlinear Fokker–Planck equation (1.3). Consequently, we realize that (1.3) involves feedback as well. We will refer to this feedback as stochastic (or statistical) feedback [67, 188, 190, 196, 387]. In particular, as we will show in Chap. 3, for strongly nonlinear Fokker–Planck equations the transport equation (1.7) applies not only for ψ1 = P (x, t) but also for ψ2 = P (x, t|x , t ), that is, for a transition probability density. One may alternatively say that for strongly nonlinear Fokker–Planck equations the transport equation (1.7) with Fˆ given by (1.8) holds for an infinitely large set of field variables ψ1 = P (x, t), ψ2 = P (x, t; x , t ), ψ3 = P (x, t; x , t ; x , t ), and so on that describe a stochastic process.

1.4 Applications

7

The basic features of a stochastic feedback system are illustrated in Fig. 1.2. There is a noise source acting on the stochastic feedback system and there are two feedback loops. The conventional feedback loop involves the state variable X of a single representative subsystem. The conventional feedback leads to transport equations of the form ∂ ψi (x, t) = Fˆ (x, ∇, t) ψi (x, t) + Ri . ∂t

(1.9)

In addition, there is a feedback loop that involves the subsystem density ρ(x). Due to this second feedback loop stochastic properties of the subsystem ensemble are fed back into the ensemble. The stochastic feedback leads to transport equations such as ∂ ψi (x, t) = Fˆ (x, ∇, t, ρ) ψi (x, t) + Ri . ∂t

(1.10)

If we use P = ρ/M0 with M0 defined such that P is normalized to unity, (1.10) can be cast into the form (1.7).

1.4 Applications There are various applications of nonlinear Fokker–Planck equations, see Table 1.2. Let us briefly address some of them. 1.4.1 Collective Phenomena Due to self-organization, many-body systems can exhibit properties that do not exist on the level of their subsystems, see Table 1.3. For example, ferromagnetic materials can show macroscopic magnetic fields. Macromolecules of liquid crystals can align themselves in a parallel fashion. In doing so, nematic phases of macroscopic orientational order can emerge. Populations of oscillatory neurons can synchronize their activity. Cross-bridges in muscle fibers can produce collective pulling forces leading to muscular contractions. Crickets can chirp in unison. Novel trends pop up in human societies every now and then and group behavior is a common feature of many societies. In these examples subsystems exhibit a collective or cooperative behavior. For this reason, we refer to the corresponding phenomena as collective or cooperative phenomena [135, 254, 267, 270, 271, 365, 546]. Collective phenomena typically involve order parameters and frequently arise due to phase transitions from phases with uncorrelated subsystem dynamics. 1.4.2 Multistable Systems In Sect. 1.2 we have discussed the notion of phase transitions. In this context, the question naturally arises: how many different phases can we observe

8

1 Introduction Table 1.2. Some applications of nonlinear Fokker–Planck equations Ref./Sect.

Condensed matter and material physics Ferromagnetism Liquid crystals (isotropic-nematic phase transition) Quantum statistics (Fermi systems, Bose systems, vortices of flow fields, grains of granular matter)

Sect. Sect. Sect. Sect. [294]

Nonlinear hydrodynamics Flows in porous media Flows in unsaturated media Polymer fluids

Sect. 6.5.1 [395] [300, 458]

(porous medium equation) (Richard’s equation) (consistent averaging, Gaussian approximation)

Plasma physics/ particle accelerator physics/ astrophysics Plasma particles (Landau form of the Fokker–Planck equation) Bunch-particles in particle beams (Vlasov–Fokker–Planck equation) Self-gravitating systems Surface physics Surface dynamics, sedimentation Wetting

(Kadar–Parisi–Zhang equation)

Statistical physics and stochastics Nonextensive thermostatistics (Tsallis entropy) Power law distributions Anomalous diffusion Synchronization Biophysics Synchronization of brain activity

(laser arrays, electronic circuitry)

(perception, memory, task related brain activity, Parkinson’s disease)

5.5.1 5.5.3 6.5.4/7 6.4.2

Sect. 7.4.1 Sect. 7.4.2 [58, 92, 94] [527] Sect. 7.5 Sect. 7.5

Chap. 6 Sect. 1.4.3, Sect. 6.5 Sect. 6.2.2, Sect. 6.5 Sect. 7.5

Sect. 5.5.2

Muscular contraction Multistable perception-action systems Population dynamics Flexibility-accuracy trade-off Ion channels of membranes

Sect. Sect. Sect. Sect. Sect.

5.5.4 5.5.6 6.5.7 7.4.4 7.5

Social behavior and psychology Behavioral synchronization (applause, fireflies flashing, chirping crickets, group behavior) Development of the self

Sect. 5.5.2 Sect. 5.5.5 [189]

Computational physics Noise generators

Sect. 7.4.3

1.4 Applications

9

Table 1.3. Examples of collective phenomena Systems

Collective phenomena Order parameter

Section

Ferromagnetic materials ferromagnetism

magnetization

5.5.1

Brains

synchronization of oscillatory activity

non-uniformity of phase distribution

5.5.2

Human societies

mass-behavior, e.g., mean normalized 5.5.2 synchronized applause harmonic correlation

Crickets

chorusing

non-uniformity of chirp distribution

5.5.2

Fireflies

rhythmic synchronous flashing

non-uniformity of flash distribution

5.5.2

Liquid crystals

nematic phase

degree of alignment 5.5.3

Muscle fibers

muscular contraction

mean cross-bridge velocity

5.5.4

order parameter

0

0

critical value

control parameter

Fig. 1.3. Bifurcation of an order parameter of a system with a monostable and a bistable parameter regime

10

1 Introduction

given a particular set of control parameter values? In general, the answer to this question depends on the system that we study. There are systems with unique stable states. Other systems have multiple stable states. Of particular interest are phase transitions that carry systems from monostable parameter regimes to multistable parameter regimes. In terms of order parameters, mono- and multistability means that order parameter equations have unique or multiple stationary solutions. A phase transition between a monostable and multistable parameter regime is illustrated in Fig. 1.3. Systems showing multistability are, for example, ferromagnets (see Sect. 5.5.1) and perceptionaction systems of humans and animals (see Sect. 5.5.6). 1.4.3 Power Law and Cut-Off Distributions Density distributions can be classified according to their qualitative shape. In particular, we may distinguish between power law distributions and cut-off distributions. Power Law Distributions Power law distributions are distinguished from other distributions by means of their long range behavior, that is, their tails. The tails of power law distributions decay according to a power law. Let ρ(x) denote a density distribution. Then, we deal with a power law distribution if for large |x| the distribution is described by ρ(x) ∝ |x|−ν

(1.11)

with ν > 0. Since in the asymptotic limit an exponential function decays faster than any power law, power law distributions do not decay as fast as exponentially decaying distributions such as Boltzmann distributions. Consequently, many-body systems described by power law distributions have subsystems that more frequently occupy unlikely states by comparison with systems described by exponentially decaying distributions. Power law distributions have been discussed in various disciplines, see Table 1.4. Famous examples of power law distributions are the Cauchy distribution and Lévy distributions. Stochastic processes related to Lévy distributions are also called Lévy flights and play an important role in many disciplines ranging from physics to economics [35, 533, 586] (see also Table 1.4). Cut-Off Distributions Cut-off distributions are finite only on subspaces of the phase spaces on which they are defined. Outside these subspaces the distributions equal zero. That is, let ρ(x) denote a density function defined on Ω. Then, cut-off distributions satisfy

1.4 Applications

11

Table 1.4. Systems exhibiting power law distributions Systems

Laws

Ref.

Earthquakes Gutenberg–Richter law [351] Pulsar bursts [95, 354] Fragmentation [413, 453, 543] Laser cooling [37] Fully developed turbulence [28, 41, 42, 43, 44, 45, 47] Linguistics Pareto’s law [587] Urban structures [507] Animal behavior [107, 612] Protein sequences Pareto’s law [306] Cell aggregation [597] Economics [67, 71, 231, 230] [402, 403, 493, 590]

density

x Fig. 1.4. A cut-off distribution of the state variable x defined on lR

ρ(x) > 0 for x ∈ A ⊂ Ω ,

ρ(x) = 0 for x ∈ Ω − A ,

(1.12)

with A = Ω. An example of a cut-off distribution is shown in Fig. 1.4. Cutoff distributions of many-body systems tell us that the subsystems of the many-body systems occupy only subspaces of phase spaces. The probability to find subsystems in states outside these subspaces is zero. Due to the decay of cut-off distributions to zero, we can say that cut-off distributions describe density and concentration fronts. Likewise, time-dependent cut-off distributions can describe distributions with moving boundaries and the propagation of concentration fronts. Therefore, they are tailored to describe, for example, density waves and the stochastic dynamics of populations. In fact, cut-off distributions have been discussed in the context of gas flow through porous

12

1 Introduction

media (Sect. 6.5.1), fluid flow in unsaturated media [395], and population dynamics (Sect. 6.5.7). Classical Solutions We will refer to infinitely differentiable solutions of Fokker–Planck equations as classical solutions. From our previous discussion it is clear that cut-off distributions are continuous functions but they are not continuously differentiable. Therefore, they do not belong to the class of classical solutions. 1.4.4 Free Energy Systems For various equilibrium systems with constant temperatures T , the distributions of stationary states (stationary distributions) correspond to the distributions that minimize the free energy F = U − T GS, where U describes the internal energy of the systems and GS denotes the Gibbs entropy [89, 509]. Nonequilibrium systems can be treated in a similar manner. To this end, one needs to employ information measures such as the Shannon information, which is (apart from a proportionality constant) equivalent to the Gibbs entropy [261, 309, 509, 518, 621]. In the context of transport phenomena, time-dependent entropy measures for single subsystem probability densities P (x, t) of many-body systems are frequently used. A famous example is the Boltzmann entropy BS[P ] = − Ω P (x, t) ln P (x, t) dM x [291, 348, 432, 576]. In due recognition of these approaches, we will consider functionals for single subsystem probability densities P (x, t) of the form F [P ] = U [P ] − QS[P ] ,

(1.13)

where U [P ] measures some kind of internal energy of a subsystem, Q denotes a noise amplitude (see Sect. 1.1.1), and S is an entropy and information measure. We will see in Sect. 4.1 that the stationary solutions of appropriately defined nonlinear Fokker–Planck equations correspond to distributions that make F extremal. Moreover, we will demonstrate that stable stationary distributions of these nonlinear Fokker–Planck equations correspond to minima (or ”valleys”) of F (see Sects. 5.1 and 5.3.2). In line with equilibrium thermostatistics, we will therefore refer to F given by (1.13) as a free energy measure. The shape of the distributions that make the free energy measures (1.13) extremal, depends on our choice of the entropy and information measure S. There are various measures S at our disposal.

Extensive Thermostatistics and µ-Space Entropies As mentioned above, a fundamental entropy measure for many-body systems is the Gibbs–Shannon entropy which is defined on many particle distributions of many-body systems (Γ -space description). If we describe many-body

1.4 Applications

13

systems in terms of one-particle or one-subsystem distributions (µ-space description), then in general we need to modify the Gibbs–Shannon entropy measure in order to account for subsystem-subsystem interactions or constraints imposed on the subsystems. For the distinction between Γ and µspace descriptions see Sect. 6.4.2. For systems with non-interacting point-like particles (e.g. the atoms of an ideal gas) for which quantum effects are irrelevant, there is no need for a modification of the Gibbs–Shannon entropy and the one-particle entropy measure is equivalent to the many-particle entropy measure. In this case, the Gibbs–Shannon entropy defined on the Γ -space gives us the famous Boltzmann entropy BS = − P (x) ln P (x) dM x that is defined on the µ-space and related to the Maxwell–Boltzmann statistics (see Sect. 4.4). In contrast, many-body systems of quantum particles such as Bose systems and Fermi systems involve quantum mechanical constraints. These constraints can be taken into account if we consider quantum mechanical entropy measures for single particle distribution that are related to quantum statistical distributions such as the Fermi–Dirac distribution and the Bose– Einstein distribution. The quantum mechanical entropy related to Fermi– Dirac distributions has also been applied to describe the statistics of vortices of flows fields. In order to account for the fact that the free phase space of many-body systems is reduced by the space occupied by subsystems (e.g., the co-volume of real gas), in the context of so-called excluded-volume theories, once more modifications of the Boltzmann entropy measure have been considered. For example, van der Waals gases, granular matter, and self-gravitating systems have been treated in the context of µ-space entropy measures, see also Table 1.5. For self-gravitating systems generalized entropy measures have also been proposed on the basis of heuristic arguments [92, 483, 527]. Table 1.5. Quantum mechanical entropies and entropies of real gases and real matter (MB=Maxwell–Boltzmann) Systems

Entropies Statistics

B MB particle systems S FD Fermi systems S BE Bose systems S FD Vortices of flow fields S FD Granular matter S van der Waals gases Self-gravitating systems

Boltzmann Fermi–Dirac Bose–Einstein Fermi–Dirac Fermi–Dirac

Ref./Sect.

Sect. 4.4 Sect. 6.5.4 Sect. 6.5.4 Sect. 6.4.2 [294] [319, 396, 408, 510, 606] [615]

14

1 Introduction

Temperature Fluctuations and Generalized Entropies Under particular circumstances it is helpful to consider the temperature of systems described by the Boltzmann entropy as a fluctuating variable. The effective statistics obtained from a Boltzmann distribution involving a fluctuating temperature variable is referred to as a superstatistics. The fluctuating temperature variable can be eliminated at the cost that we need to introduce a generalized entropy measure [42, 45, 46, 98, 440, 593]. Nonextensive Thermostatistics A popular interpretation of entropy and information measures S is that they describe the amount of chaos or the amount of disorder of systems [625]. In line with this interpretation, it is clear that the disorder of a many-body system is proportional to the size of the system provided that it is composed of non-interacting and statistically-independent subsystems (e.g. we have an ideal gas). As a result, entropy or information measures of such systems are extensive (or additive) quantities and exhibit a scaling behavior. More precisely, if we split such systems into two parts A and B, then the entropy or information S(A + B) of the whole system can be computed from S(A + B) = S(A) + S(B) ,

(1.14)

where S(A) and S(B) describe entropy or information of the parts [625]. This situation is different for many-body systems with statistically-independent but interacting subsystems. Here, we may deal with extensive measures S satisfying (1.14). Alternatively, we may deal with nonextensive (or nonadditive) measures S for which the relation S(A + B) = S(A) + S(B)

(1.15)

holds. Simple examples of many-body systems with statistically-independent but interacting subsystems are systems described by the Langevin equations defined in Sect. 3.4. If we interpret the realizations of random variables defined by these Langevin equations as the state variables of subsystems, we obtain subsystem ensembles with statistically-independent but interacting members. For details see Sect. 3.8. Nonextensive entropy and information measures are of particular relevance for thermodynamics because extensive entropy and information measures in general and the Boltzmann entropy BS in particular are subjected to severe limitations. For example, extensive thermodynamics applies to systems whose total energy is the sum of the energies of their macroscopic parts. Following Terletskii [576] and Landsberg [374], systems characterized by long range forces fail to satisfy this additivity property because interaction energies between macroscopic parts of these systems can make essential contributions to the total energy. In addition, Sharma and Garg [519] pointed out

1.4 Applications

15

that several biological and social systems should be modeled by means of nonextensive entropies and information measures. Failures of extensive thermodynamics and benefits of nonextensive thermodynamics have been nicely illustrated by means of a one-parametric entropy measure proposed by Tsallis [582], which will be addressed in Chap. 6. For reviews on this topic the reader is referred to [3, 583, 584, 587, 588, 589]. 1.4.5 Anomalous Diffusion So far, we have described systems by the number of their stationary states (e.g., unique or multiple stationary states) and the shape of their distribution functions (e.g., cut-off distributions, power law distributions, Boltzmann distributions, quantum mechanical distributions). These characteristics, however, do not provide information about the time scales on which systems evolve. Therefore, at issue is to assess how fast systems evolve with time. For this purpose, a useful measure is the variance of distributions. Let us consider the univariate case given by a random variable X(t). Then, by means of the variance K(t) = [X(t) − X(t)]2 , (1.16) one can distinguish between normal and anomalous diffusion, see Fig. 1.5. In the former case, K(t) increases linearly with time. In the latter case, there is a nonlinear increase with time. If K(t) scales slower than a linear function, we refer to the diffusion process as subdiffusive (or sublinear). Likewise, if K(t) scales faster than a linear function, we refer to the process as superdiffusive (or superlinear). A system that shows normal diffusion is a Brownian particle that evolves as d V (t) = −γV (t) + QΓ (t) , (1.17) dt where V (t) denotes the particle velocity. Then K(t) measures the mean t squared displacement with respect to the particle position X(t) = V (t ) dt and we find K ∝ t [490, 498, 619]. Anomalous diffusion has been found in various systems [70, 281, 418, 533]. For example, superdiffusion has been studied in the context of turbulent diffusion [40, 213, 287, 496, 532] and Josephson junctions [223]. Similar effects have also been found in systems of polymer-like breakable micelles [457], in two-dimensional rotating flow [541, 622], and in diffusion of atom clusters on solid surfaces [397]. Using the so-called Barenblatt–Pattle solutions, polytropic gas-flow in porous media (see Sect. 6.5.1) and surface relaxations [545] have been treated as subdiffusive stochastic processes.

16

1 Introduction

variance of a random walk

time

variance 10 0 K 1

anomalous (superdiffusive)

101 010 normal 101 01 010 anomalous 10 101 (subdiffusive) 00000000000000000 1111111111111111 10 time

Fig. 1.5. Upper panel: illustration of the increase of the variance of a random walk defined on the XY -plane. Lower panel: anomalous diffusion versus normal diffusion

1.5 Overview This book is organized as follows (see Table 1.6). In Chap. 2 fundamental definitions regarding Fokker–Planck equations will be given and several ways to classify Fokker–Planck equations will be addressed. Chap. 3 is concerned with Langevin equations. Langevin equations will be used in all subsequent chapters. Chapters 4, 5, and 6 deal with systems described by free energy measures. In Chap. 4 the focus is on transient and stationary solutions. We will derive an H-theorem for transient solutions and show how stationary solutions can be derived from the free energy principle mentioned in Sect. 1.4.4. Chap. 5 is about stability issues. In particular, phase transitions and multistability will be addressed. In Chap. 6 we will study the relationship between solutions of nonlinear Fokker–Planck equations and entropy and information measures. In this context, we will be concerned with normal and anomalous diffusion, on the one hand, and power law distributions, cut-off distributions, quantum statistical distributions, on the other hand. Chap. 7 is concerned with general nonlinear Fokker–Planck equations. Again, we will be concerned

1.5 Overview

17

with stability analysis and phase transitions. Moreover, we will address several special cases for which solution methods that are similar to those developed for the free energy case can be applied. Finally, we would like to note that some of the sections have been marked with an asterisk. They contain mathematically involved proofs of results that are used in other sections of this monograph and may be skipped by readers who are not interested in the details of these proofs. Table 1.6. Overview

Nonlinear Fokker−Planck equations Chap. 2

free energy case Chap. 4

stability Chap. 5

Langevin equations

entropy and information

Chap. 3

Chap. 6

general case Chap. 7

2 Fundamentals

2.1 Stochastic Processes Let us describe a stochastic process by means of an M -dimensional timedependent random variable X(t) defined on the phase space Ω, that is, we have X(t) = (X1 (t), . . . , XM (t)) ∈ Ω. Let us assume that X(t) is distributed like u(x) at an initial time t0 . Then, the stochastic trajectory X(t) provides us with a complete description of the process for t ≥ t0 . To see this, we note that from X(t) we can compute an infinitely large set of realizations. These realizations constitute the statistical ensemble of the stochastic process under consideration. From the statistical ensemble all quantities of interest (e.g., mean values, autocorrelations) can be obtained using ensemble averaging denoted here by . . .; X(t) ⇒ . . . . (2.1) In particular, the ensemble average with respect to the delta function δ(·) [430] gives us the probability density of X(t), P (x, t; u) = δ(x − X(t)) ,

(2.2)

which satisfies the initial condition P (x, t0 ; u) = u(x). Joint probability densities can be defined in a similar manner. For example, we have P (x2 , t2 ; x1 , t1 ; u) = δ(x1 − X(t1 ))δ(x2 − X(t2 )). By means of a hierarchy of such joint distributions, that is, by means of P (x, t; u) , P (x2 , t2 ; x1 , t1 ; u) , ... P (xn , tn ; . . . ; x1 , t1 ; u) , ...

(2.3)

with t ≥ t0 and tn ≥ tn−1 ≥ . . . ≥ t1 ≥ t0 , a stochastic process is completely defined. That is, the hierarchy (2.3) provides us with a complete description of a stochastic process. Therefore, we have two alternative descriptions of a stochastic process at hand: a stochastic process can be described by means of the random variable X(t) or by means of the hierarchy (2.3).

20

2 Fundamentals

2.2 Nonlinear Fokker–Planck Equation We can now define an evolution equation for the single time-point probability density P (x, t; u) by ∂ ∂ P (x, t; u) = − Di (x, t, P )P (x, t; u) ∂t ∂xi i=1 drift term M ∂2 + Dik (x, t, P )P (x, t; u) ∂xi ∂xk i,k=1 diffusion term M

(2.4)

with t ≥ t0 . We refer to (2.4) as a nonlinear Fokker–Planck equation because, on the one hand, the evolution equation is in general nonlinear with respect to P , and, on the other hand, for Di (x, t, P ) = Di (x, t) and Dik (x, t, P ) = Dik (x, t) it reduces to the form of the linear Fokker–Planck equation [254, 274, 498] that was originally proposed by Fokker and Planck [162, 479, 617]. In particular, we refer to Di and Dik as drift and diffusion coefficients, respectively. Accordingly, we call the two terms on the right hand side of (2.4) drift term and diffusion term. Di and Dik can depend in an arbitrary fashion on P (x, t; u). Some examples are

Di = hi (x) + wi (x − x )P (x , t; u) dM x , (2.5) Ω

Di = hi (x) + κ Xi ,

Di = Di x, ∂kn / ∂xnk , . . . dxl , t, P , Dik = Qδik P ,

Dik = δik f X 2 .

(2.6) (2.7) (2.8) (2.9)

Here, δik denotes the Kronecker symbol. We do not claim that (2.4) represents the most general form of a nonlinear Fokker–Planck equation. However, there are numerous nonlinear Fokker–Planck equations that have been discussed in the literature and can be cast into the form (2.4). In the univariate case, (2.4) reads ∂ ∂2 ∂ D2 (x, t, P )P (x, t; u) , (2.10) P (x, t; u) = − D1 (x, t, P )P (x, t; u) + ∂t ∂x ∂x2 with t ≥ t0 . Just as in the case of linear Fokker–Planck equations, one usually considers nonlinear Fokker–Planck equations with symmetric and semipositive definite diffusion coefficients. M Consequently, we will usually require that the inequalities ∀y ∈ lRM : i,k=1 Dik yi yk ≥ 0 (multivariate case) and

2.2 Nonlinear Fokker–Planck Equation

21

D2 ≥ 0 (univariate case) hold and that in the multivariate case Dik is symmetric (i.e., we have Dik = Dki ). A more detailed discussion of this issue will be given for so-called strongly nonlinear Fokker–Planck equations, see Chap. 3. Some systems are more conveniently described by means of density func tions ρ(x, t) normalized to M0 = Ω ρ(x, t) dM x; M0 may describe the total mass or the total particle number of the systems. Then, we deal with evolution equations that read as follows M M ∂2 ∂ ∂ ρ(x, t) = − dik (x, t, ρ)ρ(x, t) di (x, t, ρ)ρ(x, t) + ∂xi ∂xi ∂xk ∂t i=1 i,k=1

(2.11) in the multivariate case and ∂ ∂2 ∂ ρ(x, t) = − d1 (x, t, ρ)ρ(x, t) + 2 d2 (x, t, ρ)ρ(x, t) ∂t ∂x ∂x

(2.12)

in the univariate case. It is clear that these evolution equations can be transformed to the nonlinear Fokker–Planck equations (2.4) and (2.10) by means of P = ρ/M0 , u(·) = ρ(·, t0 ), Di (x, t, P ) = di (x, t, M0 P ) ,

Dik (x, t, P ) = dik (x, t, M0 P )

(2.13)

D1 (x, t, P ) = d1 (x, t, M0 P ) ,

D2 (x, t, P ) = d2 (x, t, M0 P ) .

(2.14)

and

2.2.1 Notation In order to ease the presentation of evolution equations for P (x, t; u), the arguments of P will be listed only in the expression with the derivative with respect to t. For example, we will write (2.4) as M M ∂ ∂2 ∂ Di (x, t, P )P + Dik (x, t, P )P . (2.15) P (x, t; u) = − ∂t ∂xi ∂xi ∂xk i=1 i,k=1

However, if we deal with evolution equations for transition probability densities P (x, t|x , t ; u), we will write out the arguments in full in order to distinguish between P (x, t|x , t ; u) and P (x, t; u) and to avoid confusion. 2.2.2 Stratonovich Form Alternatively to (2.4) one may study nonlinear Fokker–Planck equations of the form

22

2 Fundamentals

M M ∂ ∂ ˜ ∂ ∂ P (x, t; u) = − Dik (x, t, P ) P . Di (x, t, P )P + ∂t ∂xi ∂xi ∂xk i=1 i,k=1

(2.16) ˜ i (x, t, P ) = D ˜ i (x, t) and Dik (x, t, P ) = Dik (x, t) the evolution equation For D (2.16) becomes linear and corresponds to the Stratonovich form of the linear Fokker–Planck equation [221, 498]. For a state-independent diffusion matrix ˜ i . For diffusion coeffiDik , (2.4) and (2.16) are equivalent if we put Di = D cients that depend explicitly or implicitly (i.e. by means of P ) on x one can transform (2.16) into (2.4) by means of ˜ i (x, t, P ) = Di (x, t, P ) − D

M ∂Dik (x, t, P ) k=1

∂xk

.

(2.17)

2.2.3 Transient Solutions Transient solutions are time-dependent solutions of the nonlinear Fokker– Planck equation (2.4). That is, we have ∂P/∂t = 0. Of particular interest is the behavior of transient solutions in the limit t → ∞. We may distinguish between the following cases: – – –

transient solutions converge to stationary ones: limt→∞ ∂P/∂t = 0 transient solutions do not converge to stationary ones: limt→∞ ∂P/∂t = 0 transient solutions converge to solutions of stationary free energies: limt→∞ dF [P ]/dt = 0

In the latter case, F [P ] denotes the free energy of a state described by P . One caveat: while the implication ∂P/∂t = 0 ⇒ limt→∞ dF [P ]/dt = 0 holds for free energy measures F [P ] that do not explicitly depend on t, the opposite implication dF [P ]/dt = 0 ⇒ ∂P/∂t = 0 is not necessarily satisfied. We will return to this issue in Chapters 4 and 6. 2.2.4 Continuity Equation Equation (2.4) can be written as ∂ P (x, t; u) = −∇ · J(x, t, P ) , ∂t

(2.18)

where J = (J1 , . . . , JM ) is defined by Ji (x, t, P ) = Di (x, t, P )P −

M ∂ Dik (x, t, P )P . ∂xk

k=1

(2.19)

2.2 Nonlinear Fokker–Planck Equation

23

In particular, (2.10) can be written as ∂ ∂ P (x, t; u) = − J(x, t, P ) ∂t ∂x

(2.20)

with J given by J(x, t, P ) = D1 (x, t, P )P −

∂ D2 (x, t, P )P . ∂x

(2.21)

Equations (2.18) and (2.20) are referred to as continuity equations. In analogy to the theory of linear Fokker–Planck equations [254, 274, 498], we will refer to J and J as probability currents. 2.2.5 Boundary Conditions Solutions of the nonlinear Fokker–Planck equation (2.4) depend on boundary conditions. One can generalize boundary conditions defined for linear Fokker– Planck equations [221, 498] to the nonlinear case. Accordingly, we distinguish between –

natural boundary conditions: X ∈ Ω = lRM and lim|x|→∞ P (x, t; u) = 0 – periodic boundary M conditions: X ∈ Ω = i=1 [ai , bi ], bi − ai = Ti > 0, and P (. . . , xi + Ti , . . .) = P (. . . , xi , . . .) – reflective boundary conditions: M X ∈ Ω = i=1 [ai , bi ], bi > ai , and J|∂Ω = 0, where J is the probability current – mixed boundary conditions In the case of mixed boundary conditions, we have, for example, a natural boundary in combination with a reflective boundary. Furthermore, if a multivariate random vector X contains components that are subjected to boundary conditions of different kinds, we deal with mixed boundary conditions. 2.2.6 Stationary Solutions Stationary solutions of the nonlinear Fokker–Planck equation (2.4) will be denoted by Pst and satisfy ∂Pst /∂t = 0 ⇒ Pst (x, t) = Pst (x). Note that we will also refer to Pst as stationary distributions or stationary probability densities. From (2.18) we read off that stationary solutions satisfy ∇ · J(x, Pst ) = 0 .

(2.22)

That is, in the stationary case the divergence of the probability current vanishes. In the univariate case, from (2.20) it follows that ∂J/∂x = 0, which

24

2 Fundamentals

implies that J corresponds to a constant. Consequently, Pst is implicitly given by ∂ D2 (x, Pst )Pst (x) = J = const. (2.23) D1 (x, Pst )Pst (x) − ∂x The constant J is determined by the boundary conditions imposed on P . Note that in order to write (2.22) and (2.23) we have assumed that J and J given by (2.18) and (2.20) do not explicitly depend on t.

2.3 Self-Consistency Equations In many cases, from (2.22) and (2.23) implicit equations for Pst can be derived (see, e.g., (4.20) and (7.4) below). Solutions of these implicit equations can then be found by solving appropriately defined self-consistency equations. In order to elucidate this point, we assume that the stationary solutions of a multivariate nonlinear Fokker–Planck equation satisfy the implicit equation Pst (x) = f (x, Ast , α) ,

(2.24)

P (x, m) = f (x, m, α(m))

(2.25)

with Ast = Ω A(x)Pst (x) dM x. Here, A is an r-dimensional vector field A(x) = (A1 (x), . . . , Ar (x)) and α is chosen such that P is normalized to unity. We will use α = µ (chemical potential) or α = Z (partition function). Then, we define a probability density

that depends on a vector m = (m1 , . . . , mr ). Here, m denotes an independent variable and α(m) is chosen such that P is normalized to unity. Next, we define

R(m) = (2.26) A(x)P (x, m) dM x Ω

which is a function of m only. We can now define the integral equation m = R(m) .

(2.27)

If we substitute Ast = m into (2.24), where m satisfies (2.27), then we realize that (2.24) is satisfied. That is, the solutions of (2.27) determine the unknown expectation values Ai st that occur in (2.24). Therefore, the basic idea is to solve (2.27) and, subsequently, substitute the result into (2.24). Equation (2.27) is called a self-consistency equation. In deriving (2.27), we have transformed an implicit equation for a function Pst into an implicit equation for a vector m. The advantage of this procedure is that the implicit equation for m can usually be solved numerically with relatively little computation effort. Moreover, as we will see in Chapters 5 and 7 the stability of stationary solutions can also be determined by evaluating self-consistency equations.

2.5 Nonlinearity Dimension

25

Finally, note that the application of self-consistency equations is not restricted to Fokker–Planck equations with a finite nonlinearity dimension d (see Sect. 2.5 below). It can be applied to all kinds of nonlinear Fokker– Planck equations whose stationary distributions are described by implicit equations of the form (2.24).

2.4 Multistability and Basins of Attraction Self-consistency equations can have multiple solutions. If so, we obtain multiple stationary solutions of the form (2.24) with different order parameters Ast . In many cases, we can show (e.g., by means of H-theorems) that transient solutions of a nonlinear Fokker–Planck equation converge to stationary ones in the long time limit. If a Fokker–Planck equation is multistable the question arises as to which one of the stationary solutions does a transient solution converge. In other words: what are the basins of attraction of stationary distributions? We will not answer this question in general. However, there is a simple answer to this question for Fokker–Planck equations that have stationary solutions of the form (2.24) and give rise to closed evolution equations for order parameters A (t) = Ω A(x)P (x, t; u) dM x that read d A (t) = N(A) . dt

(2.28)

For every time-dependent distribution P with initial distribution u(x) and A (t0 ) = Ω A(x)u(x) dM x we obtain the corresponding stationary value Ast by solving (2.28), which, in turn, gives us the corresponding stationary solution (2.24). In short, from P (x, t0 ; u) = u we get A (t0 ). From A (t0 ) we get Ast via (2.28) and from Ast we get Pst (x, u) via (2.24). Thus, we can determine the basins of attraction of stationary solutions and write down mappings u → Pst (x, u). For examples, see Sects. 5.2.2 and 7.3.3.

2.5 Nonlinearity Dimension The probability density P of a stochastic process can be described by means of an infinitely large set of moments [221, 498]. In the univariate case, the moments read Mn = X n , (2.29) with n ≥ 1. Here, the functions X n constitute a set of linearly independent functions. Since the drift and diffusion coefficients of nonlinear Fokker– Planck equations depend on the probability density, the drift and diffusion coefficients depend in general on an infinitely large set of expectation values involving linearly independent functions. In particular, this is the case for the nonlinearity shown in (2.8). In contrast, the diffusion coefficient shown

26

2 Fundamentals

in (2.9) depends only on a single expectation value, namely, X 2 . That is, we may also deal with drift and diffusion coefficients that depend on a finite number of expectation values A1 , . . . , Ad , where A1 , . . . , Ad denote linearly independent functions. We refer to the number of expectation values that occur in the coefficients of a nonlinear Fokker–Planck equation and are related to linearly independent functions as the nonlinearity dimension d of the Fokker–Planck equation. Accordingly, for 0 < d < ∞ the univariate nonlinear Fokker–Planck equation (2.10) can be written as ∂ ∂2 ∂ D2 (x, t, A)P , P (x, t; u) = − D1 (x, t, A)P + ∂t ∂x ∂x2

(2.30)

where the vector A(x) is given by A(x) = (A1 (x), . . . , Ad (x)) and the components A1 (x), . . . , Ad (x) denote linearly independent functions. In addition, there are two extreme cases. On the one hand, we may have d = ∞ as discussed earlier. On the other hand, d = 0 means that we deal with a linear Fokker–Planck equation. That is, we regard a linear Fokker–Planck equation as a nonlinear Fokker–Planck equation that has a nonlinearity of dimension zero.

2.6 Classifications There are different ways of classifying nonlinear Fokker–Planck equations, see Fig. 2.1. First, we may distinguish between nonlinear Fokker–Planck equations to which Markov processes can be assigned and those to which Markov processes cannot be assigned or for which this issue cannot be decided. We will refer to the former kind of nonlinear Fokker–Planck equations as strongly nonlinear Fokker–Planck equations, see Chap. 3. Second, we may use free energy measures to distinguish between nonlinear Fokker–Planck equations of different kinds. If (2.4) can be written by means of a free energy functional F as ∂ δF P (x, t; u) = −∇ · [P I] + ∇ · MP · ∇ (2.31) ∂t δP we say that we deal with a free energy Fokker–Planck equation. Here, M denotes an M × M matrix and I is a drift force. If the free energy functional can be decomposed into a linear internal energy functional U0 = U (x)P dM x and an entropy or information measure S like F = U0 −QS, Ω 0 then we get ∂ δS . (2.32) P (x, t; u) = −∇ · [IP − P M · ∇U0 (x)] − Q∇ · MP · ∇ ∂t δP We will refer to nonlinear Fokker–Planck equations (2.32) as entropy Fokker– Planck equations. If S corresponds to the Boltzmann entropy and M and I do not depend on P , we obtain a linear Fokker–Planck equation. We will

2.6 Classifications

27

NLFPEs

(a)

strongly NLFPEs

linear FPE

(b)

NLFPEs free energy FPEs entropy FPEs

linear FPE

(c)

NLFPEs

d=0 0 < d
0. Then, (4.85) reads 3 3 3 ∂ ∂ ∂ ∂2 P (p, q, t; u) = − pi P + [γpi − hi (q)]P + γQ P . ∂t ∂qi ∂pi ∂p2i i=1 i=1 i=1 (4.90) From (4.90) we can see that the fluctuation strength is given by Q = γQ. 3 Equation (4.90) is referred to as Kramers equation. Using ∆p = i=1 (∂ 2 /∂p2i ), (4.90) can be written as

∂ ∂ ∂ P (p, q, t; u) = −p P + [γp − h(q)]P + Q ∆p P . ∂t ∂q ∂p

(4.91)

4.6.2 Nonlinear Case We now generalize our preceding considerations to the nonlinear case. Again, we describe a single particle defined on an M = 2M -dimensional phase space Ω spanned by the generalized coordinates q = (q1 , . . . , qM ) and momentum variables p = (p1 , . . . , pM ). That is, we have x = (p, q) ∈ Ω and P (x, t; u) → P (p, q, t; u). We write I as I = (Ip , Iq ) with Ip = Ip (p, q, t, P ) and Iq = Iq (p, q, t, P ). The mobility matrix M corresponds again to a 2M × 2M matrix M(p, q, t, P ) but now depends on P as indicated. Then, the free energy Fokker–Planck equation (4.49) becomes ∂ ∂ ∂ δF P (p, q, t; u) = − · [Ip P ] − · [Iq P ] + ∇ · MP · ∇ . (4.92) ∂t ∂p ∂q δP

4.6 Canonical-Dissipative Systems

93

Alternatively, if S is given by S = B[ Ω s(P ) dM p dM q] (see (4.5)), we have [168] ∂ ∂ ∂ δU P (p, q, t; u) = − · [Iq P ] + ∇ · MP · ∇ · [Ip P ] − δP ∂t ∂p ∂q dB ˆ s (P ) +Q ∇ · M · ∇L (4.93) dz z0 with z0 = Ω s(P ) dM p dM q. The expression ∇ · M · ∇ can be expressed pp pq qp qq using submatrices of M defined by Mlm , Mlm , Mlm , Mlm of Mik (with l, m ∈ {1, . . . , M }), which gives us [168, 193] ∂ ∂ ∂ ∂ ∂ ∂ + M pq [p, q, P ] Mik [x, P ] = M pp [p, q, P ] ∂xk ∂pl lm ∂pm ∂pl lm ∂qm ∂xi ∂ ∂ ∂ ∂ qp qq Mlm [p, q, P ] + Mlm [p, q, P ] . + ∂pm ∂ql ∂qm ∂ql (4.94) Analogously, the term ∇ · MP · ∇ can be treated. Next, we discuss two cases in which I and U are chosen such that (4.69) is satisfied. Case A In line with (4.81) and (4.82), we assume that the conservative drift forces are given by Ilp [p, q, P ] = −

∂ δU [P ] , ∂ql δP

Ilq [p, q, P ] =

∂ δU [P ] . ∂pl δP

(4.95)

Then, we have ∇·I=

∂ ∂ δU ∂ ∂ δU ∂ ∂ · Ip + · Iq = − · + · =0. ∂p ∂q ∂p ∂q δP ∂q ∂p δP

(4.96)

In addition, we have δU ∂ δU ∂ δU = Ip · + Iq · δP ∂p δP ∂q δP ∂ δU ∂ δU ∂ δU ∂ δU · + · = 0 . (4.97) =− ∂q δP ∂p δP ∂p δP ∂q δP

I·∇

That is, (4.69) is satisfied. Furthermore, the Fokker–Planck equation (4.93) reads ∂ ∂ ∂ ∂ δU [P ] ∂ δU [P ] P (p, q, t; u) = · P · P − ∂t ∂p ∂q δP ∂q ∂p δP δU dB ˆ s (P ) +∇ · MP · ∇ +Q ∇ · M · ∇L (4.98) δP dz z0 and the stationary distributions of (4.98) are given by (4.20).

94

4 Free Energy Fokker–Planck Equations

Case B Here, let us put

g˜(H)P dM p dM q ,

U [P ] = Ω

∂ H , ∂ql ∂ Ilq [p, q] = H , ∂pl

Ilp [p, q]

=−

(4.99)

where g˜(z) is a function of z and H denotes a Hamiltonian H = H(p, q). Then, one finds that the relation ∇ · I = 0 is satisfied because of (4.86). In addition, the condition I · ∇δU/δP = 0 holds provided that d˜ g /dz exists because we have δU d˜ g I·∇ = [I · ∇H] (4.100) δP dH and I · ∇H = 0. Now, the Fokker–Planck equation (4.93) reads ∂H ∂H ∂ ∂ ∂ P (p, q, t; u) = · P − · P ∂t ∂p ∂q ∂q ∂p dB ˆ s (P ) +∇ · [MP · ∇˜ g (H)] + Q ∇ · M · ∇L (4.101) dz z0 and the stationary distributions of (4.101) can be obtained from (4.20) and satisfy −1 g˜ (H(p, q)) − µ ds Pst (p, q) = (4.102) dz Q dB(z0,st )/dz with z0,st = Ω s(Pst (p, q)) dM p dM q. Example I Let us consider the energy functional

U [P (p, q)] = H0 (p, q)P (p, q) dM p dM q Ω

1 + HMF (q, q )P (p, q)P (p , q ) dM p dM q dM p dM q (4.103) 2 Ω Ω for a symmetric interaction Hamiltonian HMF . That is, we require HMF (q, q ) = HMF (q , q). Using (4.95) and (4.103), the Fokker–Planck equation (4.93) reads

4.6 Canonical-Dissipative Systems

95

∂H0 ∂ ∂ ∂H0 ∂ P (p, q, t; u) = · P − P ∂t ∂p ∂q ∂q ∂p

∂ M M M M +∇ · MP · ∇H0 + HMF (q, q )P (p , q , t; u) d p d q d p d q ∂q Ω dB ˆ s (P ) . +Q ∇ · M · ∇L (4.104) dz z0

Using (4.20) and (4.103), we conclude that the stationary distribution of (4.104) is given by −1 H0 (p, q) + Ω HMF (q − q )Pst (p , q )dM p dM q − µ ds Pst (p, q) = dz Q dB(z0,st )/dz (4.105) M M with z0,st = Ω s(Pst (p, q)) d p d q. Example II: Generalized Kramers Equation pp pq qp qq = γδlm , Mlm = Mlm = Mlm ≡ 0, and H0 = p2 /(2m) + Now, we require Mlm 2 2 V (q), where p = |p| and m > 0 describes the mass of the particle under consideration. The states of the particle are described by q = (q1 , q2 , q3 ) and p = (p1 , p2 , p3 ). Then, (4.104) becomes

∂ P (p, q, t) = ∂t

3 ∂V (q) pl ∂ ∂ γ + + HMF (q − q )P (p , q , t) d3 p d3 q P ∂pl m ∂ql ∂ql Ω l=1 3 3 ∂ pl ∂2 ˆ dB − (4.106) Ls (P ) P + γQ 3 3 ∂ql m dz ∂p2l s(P ) d p d q l=1

l=1

Ω

or ∂ P (p, q, t) = ∂t

p dV (q) ∂ ∂ 3 3 HMF (q − q )P (p , q , t) d p d q P · γ + + ∂p m dq ∂q Ω p ∂ ∂ dB ∂ ˆ − · (4.107) P (p, q, t) + γQ · Ls (P ) m ∂q dz s(P ) d3 p d3 q ∂p ∂p Ω

with Pst (p, q) = −1 2 p /(2m) + V (q) + Ω HMF (q − q )Pst (p , q ) d3 p d3 q − µ ds dz QdB(z0,st )/dz

.

(4.108)

96


For S = BS[P ] = − P ln P d3 p d3 q and V (q) = q2 /2 (4.106) can be used to describe particle bunches in particle accelerator. We will return to this issue in Sect. 7.4.2. Example III We consider (4.101) for particles with position and momentum vectors q = pp (q1 , q2 , q3 ) and p = (p1 , p2 , p3 ). In addition, we put Mlm = γδlm , γ > 0, pq qp qq and Mlm = Mlm = Mlm = 0, where γ can be seen as a friction coefficient, see (4.109) below. In order to make contact with other z studies (e.g. [149]), we introduce the function g(z) = d˜ g /dz ⇒ g˜(z) = 0 g(z ) dz . Then, from (4.94) and (4.101) we obtain ∂ ∂ P (p, q, t) = ∂t ∂pl 3

l=1

∂H0 ∂H0 + γg(H0 ) ∂ql ∂pl

dB +γQ dz Ω

3 ∂ ∂H0 P − P ∂ql ∂pl l=1

3 ∂2 ˆ Ls (P ) , 3 3 ∂p2l s(P ) d p d q

(4.109)

l=1

and stationary solutions are determined by ⎫ ⎧ H0 ⎪ ⎪ −1 ⎪ g (z) dz − µ ⎪ ⎬ ⎨ ds . Pst (p, q) = ⎪ ⎪ dz Q dB/dz ⎪ ⎪ ⎭ ⎩

(4.110)

Equation (4.109) can be regarded as a generalization of the linear Fokker– Planck equations of canonical-dissipative systems as discussed in [149, 516] and may be written as ∂ ∂ ∂H0 ∂H0 ∂ ∂H0 · · P − P (p, q, t) = + γg(H0 ) P ∂q ∂p ∂p ∂p ∂q ∂t dB ∂ ∂ ˆ (4.111) · Ls (P ) , +Q dz s(P ) d3 p d3 q ∂p ∂p Ω with Q = γQ.

4.7 Boundedness of Free Energy Functionals∗ So far, we have assumed that the free energy measures of interest are bounded from below, see (4.3). Our objective now is to derive sufficient conditions for the boundedness of free energy functionals [175].

4.7 Boundedness of Free Energy Functionals∗

97

4.7.1 Distortion Functionals Distortion functionals relate stationary solutions of nonlinear Fokker–Planck equations in general and free energy Fokker–Planck equations in particular to Boltzmann distributions and are helpful tools to investigate the boundedness of free energy measures. We will consider here distortion functionals related to free energy measures, whereas in Chap. 7 we will be concerned with distortion functionals of a more general type. The distortion functional G related to free energy measures F given by (4.1) and (4.2) is defined by [166, 190, 192, 193, 199] δS 1 δUNL G[u] = exp − −1+ . (4.112) δu Q δu Let us express the variational principle δF/δP = µ as δS 1 δU 1 δUNL U0 (x) + = −µ = −µ . δPst Q δPst Q δPst

(4.113)

Then, (4.113) can be written as [U0 (x) − µ] 1 δUNL δS −1 . G[Pst ] = exp − = exp − −1+ δPst Q δPst Q (4.114) Using the Boltzmann distribution W (x) =

exp{−U0 (x)/Q}

(4.115)

exp{−U0 (x)/Q} dM x Ω

(see also Sect. 4.4), we obtain the mapping Pst → W defined by G[Pst ] =

1 W (x) . Z

(4.116)

Here, Z is a normalization constant that is implicitly determined by the normalization condition Ω Pst (x) dM x = 1. 4.7.2 Kullback Measure and Entropy Inequality Let us consider an entropy or information measure S[P ] that satisfies the concavity inequality S[P ] ≤ S[P0 ] + δS[P0 ](P − P0 ) ,

(4.117)

for P, P0 > 0, where the equal sign holds only for P = P0 (for properties of S such as concavity see Sect. 6.4.1). Equation (4.117) can be written as

98


S[P0 ] − S[P ] + δS[P0 ](P − P0 ) ≥ 0 .

(4.118)

On the basis of the inequality (4.118), we define the semi-positive definite measure [167, 168, 192] K[P, P0 ] = S[P0 ] − S[P ] + δS[P0 ](P − P0 ) ≥ 0 .

(4.119)

The functional K takes two arguments: P and P0 . It can be regarded as a distance measure. That is, it measures the difference between the probability densities P and P0 . If P equals P0 we have K = 0. If P differs from P0 we have K > 0: K > 0 ⇔ P = P0 , K = 0 ⇔ P = P0 . (4.120) We refer to K as a general Kullback measure because it recovers the Kullback distance measure in the case of the Boltzmann entropy (see below). Our considerations reveal that the general Kullback measure is nothing but the concavity inequality of entropy and information measures: Kullback measure ⇔ concavity of entropies and information measures. (4.121) Note that the Kullback measure (4.119) can also be defined for two discrete (0) probability distributions {pi } and {pi } and entropy measures of the form S = S(p1 , . . . , pN ): N 9 : ∂S (0) (0) (0) K {pi }, {pi } = S({pi }) − S({pi }) + (pi − pi ) , (0) ∂p i {pi }={p } i=1 i (4.122) N see also [185] for the special case S = i=1 s(pi ). Boltzmann–Kullback Measure For the Boltzmann entropy BS[P ] = − Ω P ln P dM x, the Kullback measure (4.119) reads

B K[P, P0 ] = − P0 ln P0 dM x Ω

+ P ln P dM x − [1 + ln P0 ](P − P0 ) dM x Ω

Ω P M = d x. P ln (4.123) P0 Ω This measure is known in the literature as the Kullback measure or the Kullback distance measure [257, 361, 362]. In what follows, we will refer to B K[P, P0 ] as the Boltzmann–Kullback measure. Since the Boltzmann entropy satisfies the concavity inequality (4.117), the measure BK is semi-positive definite. We would like to present here also an alternative proof of this property.


99

We start off with the logarithm ln(x). The logarithm satisfies ln(1) = 0. Furthermore, if we plot ln(x) and x − 1 in one diagram, we see that the inequality ln(x) ≤ x − 1 (4.124) holds for x > 0, where the equal sign holds for x = 1 only. Now, let us replace x by P0 (x)/P (x) for P, P0 > 0. Then, we conclude that P0 P0 ≤ ln −1 P P P0 ≤ P0 − P ⇒ P ln P

P0 dM x ≤ 0 ⇒ P ln P Ω

P B ⇒ K[P, P0 ] = dM x ≥ 0 . P ln P 0 Ω (4.125) Note that in the derivation above we used the normalization condition of probability densities in terms of Ω [P0 − P ] dM x = 0. General Kullback Measure for Stationary Probability Densities In particular, the general Kullback measure can be used to compare arbitrary probability densities P with stationary probability densities Pst obtained from the free energy principle. In this case, we put P0 = Pst and (4.119) becomes K[P, Pst ] = S[Pst ] − S[P ] + δS[Pst ](P − Pst ) .

(4.126)

If we multiply (4.113) with a function f (x) and integrate with respect to x, we obtain δS[Pst ](f ) = δU [Pst ](f )/Q − µ Ω f (x) dM x. In particular, for f = P − Pst we obtain

1 µ [P − Pst ] dM x . (4.127) δS[Pst ](P − Pst ) = δU [Pst ](P − Pst ) − Q Q Ω =0 Consequently, (4.126) becomes K[P, Pst ] =

1 δU [Pst ](P − Pst ) − S[P ] + S[Pst ] ≥ 0 . Q

(4.128)

Using (4.2) and δU [Pst ](P − Pst ) = δUNL [Pst ](P − Pst ) + UL [P ] − UL [Pst ], which implies

100


δU [Pst ](P − Pst ) = δUNL [Pst ](P − Pst ) + U [P ] − U [Pst ] − (UNL [P ] − UNL [Pst ]) , (4.129) we can write (4.128) as Q K[P, Pst ] = F [P ] − F [Pst ] + δUNL [Pst ](P − Pst ) − (UNL [P ] − UNL [Pst ]) . (4.130) 4.7.3 Generic Cases and Schl¨ ogl’s Decomposition of Kullback Measures Linear Energy Functionals The result (4.130) suggests that we examine in more detail the case in which energy functionals can be written as U = UL = Ω U0 (x)P (x) dM x. Then, (4.130) becomes Q K[P, Pst ] = F [P ] − F [Pst ] (4.131) or K[P, Pst ] = − (S[P ] − S[Pst ]) +

1 (U [P ] − U [Pst ]) . Q

(4.132)

For the special case of the Boltzmann entropy, this relation between the Kullback measure, on the one hand, and the energy and entropy terms, on the other hand, has been discussed, for example, by Schl¨ ogl [508, 509]. Equation (4.132) demonstrates that Schl¨ ogl’s relationship is not a peculiarity of the Boltzmann entropy but holds for all kinds of Kullback measures K, entropy and information measures S, and linear internal energy functionals U [167]. From the semi-positivity of K it follows that F [P ] ≥ F [Pst ] .

(4.133)

If F [Pst ] is finite, we can draw the conclusion that F [P ] is bounded from below. Furthermore, it is clear from (4.133) that for linear functionals U and concave measures S stationary distributions given by the free energy principle δF/δP = µ correspond to minima of F . In terms of the so-called Massieu potential U [P ] , (4.134) J[P ] = S[P ] − Q K can also be written as the difference K[P, Pst ] = −(J[P ] − J[Pst ]) .

(4.135)

Negative Concave Energy Functionals We consider now a negative concave (or convex) energy functional U . Then, U satisfies the convexity inequality


U [P ] ≥ U [P0 ] + δU [P0 ](P − P0 ) ,

101

(4.136)

see also (4.117). In particular, for P0 = Pst we have U [P ] ≥ U [Pst ] + δU [Pst ](P − Pst ) ⇒ δU [Pst ](P − Pst ) ≤ U [P ] − U [Pst ] .

(4.137)

Consequently, from (4.128) we obtain 0 ≤ K[P, Pst ] 1 = δU [Pst ](P − Pst ) − S[P ] + S[Pst ] Q 1 ≤ (U [P ] − U [Pst ]) − S[P ] + S[Pst ] . Q

(4.138)

Just as in the case of linear energy functionals, we arrive at the result F [P ] ≥ F [Pst ] ,

(4.139)

which implies that F is bounded from below provided that F [Pst ] is finite. Nonlinear Energy Functionals in Finite Phase Spaces We consider systems with random variables defined on finite phase spaces Ω. We assume that the kernel of the functional U and the kernel of the functional δU [P ](P ) are continuous functions. Then, these kernels are bounded from below and from above on the phase space Ω. Usually, we will then deal with functionals U [P ] and δU [P ](P ) that are bounded like |U [P ]| < C1 ,

|δU [P ](P )| < C2 .

(4.140)

For example, for U0 ∈ C 0 (Ω) and P ∈ C 0 (Ω) the integral Ω U0 (x)P (x) dM x is larger than or equal to minx∈Ω {U0 (x)} and smaller than or equal to maxx∈Ω {U0 (x)}. Assuming that (4.140) holds, from (4.128) we obtain 0 ≤ K[P, Pst ] 1 δU [Pst ](P ) − δU [Pst ](Pst ) Q C2 ≤ S[Pst ] − S[P ] + 2 Q 1 1 C2 1 = S[Pst ] − U [Pst ] − S[P ] + U [P ] + 2 + (U [Pst ] − U [P ]) Q Q Q Q 1 C1 + C2 ≤ (F [P ] − F [Pst ]) + 2 . (4.141) Q Q = S[Pst ] − S[P ] +

Consequently, if the integral F [Pst ] exists (which is usually the case due to the finiteness of Ω), then F [P ] is bounded from below:

102


F [P ] ≥ F [Pst ] − 2(C1 + C2 ) .

(4.142)

The boundedness of free energy measures of systems with finite phase spaces can also be shown in an alternative fashion [172]. Let us consider a phase space M M Ω with Ω dM x = V < ∞ (e.g., Ω = i=1 [ai , bi ] ⇒ V = i=1 (bi − ai )). Let U [P ] be bounded from below by U [P ] ≥ Umin . Furthermore,we assume that S is maximal for the uniform distribution: Smax = S(P = 1/ Ω dM x = 1/V ). Then, we obtain F [P ] = U [P ] − QS[P ] ≥ Umin − Q Smax .

(4.143)

Classical Mean Field Energy Functionals and Boltzmann Statistics Of particular interest are systems that exhibit, on the one hand, Boltzmann statistics (i.e., Boltzmann distributions) and, on the other hand, involve energy functionals that are of second order with respect to probability densities (such functionals are typically found in systems with mean field interactions). That is, we assume now that S = BS = − Ω P ln P dM x and

1 U= U0 (x)P (x) dM x + UMF (x, y)P (x)P (y) dM x dM y . (4.144) 2 Ω Ω Ω We assume that the interaction potential UMF satisfies the symmetry condition UMF (x, y) = UMF (y, x). The distortion functional (4.112) reads

1 M UMF (x, y) u(y) d y . (4.145) G[u] = u exp Q Ω We define now the functional I given by

1 I[P, P0 ] = − UMF (x, y)P (x)P (y) dM x dM y 2Q Ω Ω

G(P ) dM x P (x) ln + G(P ) 0 Ω

(4.146)

that involves two probability densities P and P0 [166, 199]. For UMF = 0 we have G[u] = u and, consequently, I[P, P0 ] reduces to the Boltzmann–Kullback measure (4.123). Equation (4.146) can alternatively be expressed as

1 UMF (x, y)P (x)P (y) dM x dM y I[P, P0 ] = 2Q Ω Ω

P + dM x . P (x) ln (4.147) G(P0 ) Ω The integral (4.147) can be used to compare stationary probability densities obtained from the free energy principle with arbitrary probability densities


103

P . To this end, we put P0 = Pst , where Pst satisfies (4.116). That is, we replace G(P0 ) by G(Pst ) = W/Z and obtain

1 UMF (x, y)P (x)P (y) dM x dM y I[P, Pst ] = ln Z + 2Q Ω Ω

P + dM x . P (x) ln (4.148) W Ω B K[P, W ] ≥ 0 Note that Z is the normalization constant of Pst . We assume that the mean field potential UMF is bounded from below by UMF (x, y) ≥ C which implies that the ensemble average f (x) = Ω UMF (x, y)P (y)dM y is bounded from below by C. This result, in turn, implies that the ensemble average f (x)P (x) dM x is bounded from below by C. Consequently, the double Ω integral occurring in (4.148) is bounded from below by C/(2Q) and from (4.148) we obtain C I[P, Pst ] ≥ ln Z + . (4.149) 2Q That is, I[P, Pst ] is bounded from below. In addition, the functional I[P, Pst ] is, up to a constant, equivalent to F [P ]/Q. The reason for this is that B K[P, W ] can be written as BK[P, W ] = − BS[P ] − Ω P (x) ln W (x) dM x. Using (4.115) for U (x) = U0 (x) and ZB = Ω exp{−U0 (x)/Q} dM x, we can write BK[P, W ] as BK[P, W ] = − BS[P ] + Q−1 Ω P (x)U0 (x) dM x + ln ZB . Substituting this result into (4.148) gives us I[P, Pst ] = ln(ZB Z) − BS[P ] +

U [P ] Q

(4.150)

or, alternatively, the final result: I[P, Pst ] =

1 F [P ] + ln[ZB Z] . Q

(4.151)

Comparing (4.149) and (4.151), we obtain C . (4.152) 2 The inequality (4.152) states that if we deal with systems that exhibit Boltzmann statistics and involve classical mean field interaction functionals that are bounded from below, then we have free energy measures that are bounded from below as well. This result holds for mean field systems defined on all kinds of phase spaces. While for systems defined on finite phase spaces we have derived the same result under much weaker conditions in the previous paragraph, the estimate (4.152) can in particular be used for systems defined on infinite phase spaces (e.g., Ω = lRM ) and mixed phase spaces (e.g. M Ω = lRM × i=1 [ai , bi ] with M + M = M such as phase oscillator systems with inertia terms). F [P ] ≥ −Q ln(ZB ) +

104


Nonlinear Energy Functionals and Boltzmann Statistics Here, we assume that we deal with the Boltzmann statistics and a general nonlinear energy functional U composed of a linear part UL and a nonlinear part UNL , see (4.2). Then, G is given by 1 δUNL G[u] = u exp , (4.153) Q δu see (4.112). With (4.153) at hand, we can generalize the functional (4.146) to

G(P ) M I[P, P0 ] = . (4.154) d x dP ln G(P0 ) Ω The expression dP . . . denotes a functional integration, that is, an integration with respect to a function. We interpret the functional I as a functional that satisfies a particular ordinary first order differential equation. To this end, we introduce a real parameter κ and consider a probability density P˜ (x, κ) depending on κ. Then, the integral (4.154) is defined as the integral I[P˜ , P0 ] that satisfies 7 6

d ˜ dP˜ G(P˜ ) dM x . (4.155) I[P (x; κ), P0 ] = ln dκ dκ G(P ) 0 Ω For P0 = Pst the term G(P0 ) can be replaced by G(Pst ) = W/Z. Analogously to the derivation of (4.151), we then conclude that

dP˜ dP˜ d ˜ I[P , Pst ] = ln[G(P˜ )] dM x + ln (ZB Z exp{U0 /Q}) dM x dκ Ω dκ Ω dκ 6 7

˜] d 1 d [ P U NL B ˜ = − S[P ] + + U0 (x) P˜ dM x . (4.156) dκ Q Q dκ Ω Next, we integrate both sides of (4.156) with respect to κ. Subsequently, we drop the parameter κ (that has merely been used to carry out the functional integration using standard techniques). The result reads:

1 G(P ) M I[P, Pst ] = = F [P ] + I0 , d x dP ln (4.157) G(P ) Q st Ω where I0 denotes an integration constant. Since F [P ] can be decomposed into F = UNL − Q BS + UL and UL can be written as

M UL = U0 (x)P (x) d x = −Q P (x) ln[ZB W (x)] dM x , (4.158) Ω

Ω

we can write F as F = UNL − Q ln ZB + Q Ω P ln[P/W ] dM x. Due to the semi-positivity of the Boltzmann–Kullback measure (i.e., because of


105

P ln[P/W ] dM x ≥ 0), we conclude that if the nonlinear energy functional is bounded from below by UNL,min , then the free energy functional F and the functional I are bounded from below as well: Ω

F [P ] ≥ −Q ln ZB + UNL,min , UNL,min + I0 . I[P, Pst ] ≥ ln ZB + Q

(4.159) (4.160)

Finally, we would like to mention that from (4.153) and (4.154) and the relation Ω dM x[ dP δUNL /δP ] = UNL [P ] (see below), it follows that I[P, P0 ] can equivalently be expressed as

1 P dM x + I0 . P (x) ln (4.161) I[P, P0 ] = UNL [P ] + Q G(P ) 0 Ω The functional (4.161) generalizes the functional (4.147). Likewise, as stated earlier, (4.154) contains (4.146) as a special case. In order to see this, note that the functional Y [P ] = 0.5 Ω Ω UMF (x, y)P (x)P (y) dM x dM y with UMF (x, y) = UMF (y, x) satisfies Ω Ω P Y [δY /δP ]dM x dM y = δY [P ](P ) = 2Y [P ] with δY /δP = Ω UMF (x, y)P (y) dM y. Consequently, for UNL = Y we can add on the right-hand side of (4.161)a zero in the form of 0 = −2Q−1 Y + Q−1 δY [P ](P ) and write Q−1 Y [P ](P ) as Ω P ln[exp{Q−1 δY /δP }] dM x which yields

1 P exp{Q−1 δY /δP } dM x + I0 . (4.162) P (x) ln I[P, P0 ] = − Y + Q G(P ) 0 Ω and corresponds to (4.146) for I0 = 0. Functional Integration Let f (x) by a function defined on a one-dimensional domain Ω. Then, z=f (x) dx[ df g(f (x))] can be written as Ω g(z)dz dx. That is, we inΩ tegrate with respect to z, replace in the result thus obtained the variable z by f (x), and finally integrate with respect to x. It is clear from the notion of a functional integration that the functional integration and the functional derivative can the be regarded as inverse operations. For example, functional Y [f ] = Ω dx[ df g(f (x))] can be written as Y [f ] = dxH(f ) f with H(f ) = df g(f ), which implies that δY = dx[dH/df ]δf and δY /δf = dH/df = g(f ). This finally leads to Y [f ] = Ω dx[ df δY /δf ]. Nonlinear Free Energy Functionals with Matching Condition We consider a system with a nonlinear energy functional U given by (4.2) and an arbitrary entropy and information measure S. We assume that the system

106


has at least one stationary state for which the free energy F = U − QS and the nonlinear part UNL of the energy measure are stationary: δF [Pst ] = 0 and δUNL [Pst ] = 0. In this case, from (4.130) and K ≥ 0 it follows that F [P ] ≥ F [Pst ] − UNL [Pst ] + UNL [P ] .

(4.163)

Assuming that the nonlinear part UNL of the internal energy is bounded from below like UNL [P ] ≥ UNL,min , we obtain F [P ] ≥ F [Pst ] − UNL [Pst ] + UNL,min .

(4.164)

That is, if the integrals F [Pst ] and UNL [Pst ] exist (i.e., are finite), then the free energy F is bounded from below. Summary Let us summarize the results obtained so far. We have examined the boundedness of free energy measure for several generic cases. The conditions involved in these cases as well as the results are listed in Table 4.2. We conclude that there are a few essential ingredients that lead to the boundedness of free energy functionals. For systems described by finite phase spaces the boundedness results from the following assumptions: (i) energy measures are continuous and, therefore, bounded from below and above and (ii) stationary states exist with finite free energies. Alternatively, free energies are bounded if the following assumptions hold: (i) internal energy measures are bounded from below and (ii) entropy and information measures exhibit a global maximum (which is usually assumed for the uniform distribution). For systems defined on infinite phase spaces the boundedness of free energy measures is, roughly speaking, a consequence of the following properties: (i) energy measures are bounded from below, (ii) entropy and information measures are concave measures, and (iii) there exists at least one stationary state with finite values for internal energy, entropy or information, and free energy.

4.8 First, Second, and Third Choice Thermostatistics

107

Table 4.2. Boundedness of several generic free energy functionals of the form F = U − QS (f.b. = from below, f.a. = from above, ∞ = infinite phase space, UL =linear energy functional)

Generic S type A B C D E F G

general general general general B S

U

U = UL negative concave bounded f.b. & f.a. bounded f.b. U = UL + UMF , UMF bounded f.b. B S U = UL + UNL , UNL bounded f.b general U = UL + UNL , matching condition

Ω

finite/∞ finite/∞ finite finite finite/∞

K, I F[P]

K K K – I

bounded bounded bounded bounded bounded

F [Pst ]

f.b. f.b. f.b. f.b. f.b.

minimal minimal – – –

finite/∞ I

bounded f.b. –

finite/∞ K

bounded f.b. –

4.8 First, Second, and Third Choice Thermostatistics In the preceding section we have considered internal energy functionals such as

U [P ] = U0 (x)P (x) dM x , Ω

1 M U [P ] = U0 (x)P (x) d x + UMF (x, y)P (x)P (y) dM x dM y . 2 Ω Ω Ω (4.165) Functionals of this kind can be generalized by replacing P with a function of P , say, f (P ):

U [P ] = U0 (x)f [P (x)] dM x , Ω

1 M U [P ] = U0 (x)f [P (x)] d x + UMF (x, y)f [P (x)]f [P (y)] dM x dM y . 2 Ω Ω Ω (4.166) Alternatively, we may replace P by f (P )/ Ω f (P ) dM x, which gives us internal energy functionals that read as U0 (x)f [P (x)] dM x , U [P ] = Ω f (P ) dM x Ω

108


U [P ] =

Ω

U0 (x)f [P (x)] dM x + f (P ) dM x Ω

Ω

Ω

UMF (x, y)f [P (x)]f [P (y)] dM x dM y . 2[ Ω f (P ) dM x]2 (4.167)

In particular, if we deal with entropy and information measures that involve power laws it has been suggested to consider internal energy functionals with f (z) = z q . In this context, thermostatistics based on internal energy measures of the form (4.165), (4.166), and (4.167) have been called first, second, and third choice thermostatistics, respectively [106, 592], and have attracted considerable interest [2, 136, 202, 613, 641]. Moreover, the expres sion P = P q / Ω P q dM x that occurs in the third choice thermostatistics for f (z) = z q is known as the escort distribution of P [3, 48].

5 Free Energy Fokker–Planck Equations with Boltzmann Statistics

In Sect. 4.4 we have considered systems with linear internal energy functionals that exhibit Boltzmann statistics. In this chapter we will again consider systems that exhibit Boltzmann statistics but as opposed to Sect. 4.4 we will discuss nonlinear internal energy functionals. The nonlinear energy terms are assumed to reflect subsystem-subsystem interactions (see Sect. 1.1.2). That is, we are now concerned with many-body systems that involve interacting subsystems and exhibit Boltzmann statistics. Free energy measures of this kind of system read

F [P ] = U0 (x)P (x) dM x + UNL [P ] − Q BS[P ] , (5.1) Ω B

where S denotes the Boltzmann entropy

B S[P ] = − P ln P dM x

(5.2)

(see Sect. 6.4.2). We assume that UNL [P ] is bounded from below like UNL [P ] ≥ UNL,min . We further assume that the evolution of P (x, t; u) for t ≥ t0 is given by the free energy Fokker–Planck equation δF ∂ P (x, t; u) = ∇ · P ∇ , (5.3) ∂t δP see (4.4), which can equivalently be expressed as ∂ δUNL [P ] P (x, t; u) = ∇ · ∇U0 (x) + ∇ P + Q ∆P . δP ∂t

(5.4)

We restrict ourselves to considering systems for which stationary solutions can be obtained from the free energy principle (4.17). Since the entropy kernel of BS is given by s(z) = −z ln z, we have ds/dz = − ln z − 1 and [ds/dz]−1 = exp{−z−1}. In addition, the outer function B(z) of BS simply reads B(z) = z. Consequently, (4.20) becomes U0 (x) + δUNL [Pst ]/δP 1 Pst (x) = exp − , (5.5) Z Q where Z denotes a normalization constant given by ln Z = 1 − µ/Q (see also Sect. 4.4).

110


Finite Dimensional Nonlinearities In order to evaluate the implicit equation (5.5), we consider nonlinear Fokker–Planck equations with finite dimensional nonlinearities (i.e., we have d < ∞, see Sect. 2.6). In this case, the functional derivative δUNL [P ]/δP can as a function of x and a set of expectation values A = be regarded A(x)P (x) dM x with A(x) = (A1 (x), . . . , Ad (x)): Ω δUNL [P ] δUNL = (x, A) . δP δP

(5.6)

The expectation values may be regarded as order parameters (see Sect. 1.2). Equations (5.4) and (5.5) can now be written as ∂ δUNL P (x, t; u) = ∇ · ∇U0 (x) + ∇ (x, A) P + Q ∆P (5.7) ∂t δP and

⎧ ⎫ δUNL ⎪ ⎪ ⎨ ⎬ U (x, A (x) + ) 0 st 1 δP . Pst (x) = exp − ⎪ ⎪ Z Q ⎩ ⎭

(5.8)

Equation (2.25) reads ⎧ ⎫ δUNL ⎪ ⎪ ⎨ ⎬ U (x, m) (x) + 0 1 δP , P (x, m) = exp − ⎪ ⎪ Q Z ⎩ ⎭ with Z given by Z(m) = ing (2.26) in the form of

Ω

(5.9)

exp {−{U0 (x) + δUNL /δP (x, m)}/Q} dM x. Us

A(x)P (x, m) dM x ,

R(m) =

(5.10)

Ω

we define the self-consistency equation m = R(m) .

(5.11)

As shown in Sect. 2.3, solutions of the self-consistency equation (5.11) determine the order parameter values Ast . That is, solving (5.11) and substituting Ast = m into (5.8) gives us the stationary solutions of the free energy Fokker–Planck equation (5.7).

5.1 Stability Analysis In the context of nonlinear Fokker–Planck equations it is useful to distinguish between different kinds of stationary distributions: unstable, stable and

5.1 Stability Analysis

111

asymptotically stable ones. The basic idea is to adopt the stability analysis of deterministic systems [379, 610] in order to determine the stability of stationary distributions of nonlinear Fokker–Planck equations. In line with this idea we will determine the stability of stationary distributions by studying the evolution of transient solutions that correspond to perturbed stationary distributions. In what follows, we will restrict our attention to Fokker–Planck equations with coefficients that do not explicitly depend on time. Let Pst (x) denote a stationary probability density. Let P (x, t; u) denote a time-dependent probability density that is at t = t0 in some kind of neighborhood of Pst : u ≈ Pst . Then, we denote by (x) the perturbation given by = P (x, t0 ) − Pst . The function is assumed to be a small quantity. We refer to a stationary probability density as asymptotically stable if all perturbations of the probability density vanish: ∀ : lim P (x, t, Pst + ) = Pst (x) ⇒ Pst = asymptotically stable t→∞

(5.12)

(see also Fig. 5.1a). We refer to a stationary probability density as stable if all perturbations remain in a neighborhood of the probability density. A special case of a stable stationary probability density is a distribution Pst , for which perturbations vanish or give rise to further stationary distributions Pst : 1 2 ∀ : lim P (x, t; Pst + ) = Pst (x) or [Pst (x) = Pst (x) + ] t→∞

⇒ Pst = stable

(5.13)

(see also Fig. 5.1b). Finally, we refer to a stationary probability density as unstable if the probability density is not stable. In other words, a stationary probability density Pst is unstable if there exist perturbed distributions P = Pst + that leave the neighborhood of Pst no matter how small we choose the perturbation . In line with this notion, a sufficient condition for Pst to be an unstable distribution is given by ∃ : lim P (x, t; Pst + ) = Pst (x) , Pst (x) = Pst (x) + dχ(x) t→∞

⇒ Pst = unstable.

(5.14)

Equation (5.14) states that Pst is unstable if there are perturbations of Pst for which P (x, t; Pst +) converges to a stationary probability density Pst that is significantly different from Pst although can be chosen arbitrarily small. By significantly different we mean that Pst is not in some kind of neighborhood of Pst and cannot be derived from Pst by means of a perturbation dχ of Pst (see also Fig. 5.1c). In some cases, a norm · for the perturbations of stationary probability densities can be found. By means of the evolution of this norm, one can then determine the stability of stationary distributions as well. For example, if for all (nonvanishing) small deviations the norm decreases with time, then

112


(b) Pst

P st + ε

(a)

(c) Pst

Pst P st + ε

Pst/

P st + ε

function space of distributions Fig. 5.1. Examples of stationary distributions Pst : an asymptotically stable distribution (panel (a)), a family of stable distributions (panel (b)), and an unstable distribution (panel (c)). The circles define neighborhoods of the stationary distributions. In panel (b) the line with the dots describes a continuous family of stationary distributions (the dots represent the stationary distributions of the family and actually are located infinitely close to each other)

for t → ∞ we have = 0 ⇒ P = Pst and, consequently, Pst is asymptotically stable: d ∀ : (5.15) < 0 ⇒ Pst = asymptotically stable. dt In contrast, if for all perturbations the norm increases with time, then we conclude that Pst is unstable; d (5.16) > 0 ⇒ Pst = unstable. dt Let us determine next the stability of the stationary distributions by means of Lyapunov’s direct method, linear stability analysis, and self-consistency equation analysis [135, 172, 176, 187, 198, 199, 365, 522, 523, 526, 527]. ∀ :

5.1.1 Lyapunov’s Direct Method Lyapunov’s direct method for deterministic systems [379, 610] can be adopted to examine evolution equations for probability densities P [172, 176, 187, 199, 249, 522, 523, 526, 527]. Accordingly, Lyapunov’s direct method can be applied to evolution equations for P for which a functional F [P ] exists that satisfies d d ∂ F ≥ Fmin , (5.17) F ≤0, F =0⇔ P =0. dt dt ∂t In this case, F is referred to as the Lyapunov functional, see Sect. 4.3. In the case of free energy Fokker–Planck equations this requirement is satisfied (see (4.29)) and the Lyapunov functional corresponds to a free energy measure.


113

Let us consider perturbations (x) of a stationary distribution Pst (x). If δ 2 F [Pst ]() > 0 for all = 0, then Pst corresponds to a minimum of F . From δF [Pst ]/δP = µ ⇒ δF [Pst ]() = 0 and δ 2 F [Pst ]() > 0, we conclude that for small perturbations and we have δF [Pst + ]( ) = 0. That is, for small there does not exist a probability density P = Pst + that corresponds to another stationary point of F and describes a further stationary solution of the Fokker–Planck equation. Since from (5.17) we have ∂P/∂t = 0 ⇒ dF/dt < 0 we conclude that every perturbed stationary solution P = Pst + evolves in such a way that the inequality dF/dt < 0 is satisfied as long as = 0. Since P = Pst + is located in a neighborhood of a minimum of F , the time-dependent solution P cannot leave this neighborhood (because this would imply an increase of F ). The only behavior of the solution P = Pst + that is consistent with the constraint dF/dt < 0 for = 0 and the fact that P is located (in the function space of probability densities) in a neighborhood of a minimum of F is the relaxation to the unperturbed state described by Pst . Therefore, we get ∀ = 0 : δ 2 F [Pst ]() > 0 ⇒ Pst = asymptotically stable.

(5.18)

Let Pst correspond to a maximum or a saddle point of F such that there is at least one small perturbation which yields δ 2 F [Pst ]() < 0. Then, the inequality F [Pst + ] < F [Pst ] holds and the time-dependent probability density P (x, t; u) with u = Pst + at t = t0 cannot return to Pst (x) for any t ≥ t0 (because F cannot increase and F (t0 ) < F [Pst ]). Since the system under consideration has a Lyapunov functional the H-theorem discussed in Sect. 4.3 applies and the system converges to a stationary distribution Pst . If Pst corresponds to a maximum of F , then there cannot exist another stationary distribution in a neighborhood of Pst , which implies that Pst must be significantly different from Pst . If Pst corresponds to a saddle point of F , then one often can show again that Pst must be significantly different from Pst . Therefore, usually, the implication (5.14) holds and we obtain: ∃ : δ 2 F [Pst ]() < 0 ⇒ Pst = unstable.

(5.19)

In sum, the sign of the second variation of the free energy F determines the stability of stationary distributions. For F given by (5.1) the second variation reads

δ 2 UNL [Pst ] 2 M M M 2 δ F [Pst ]() = d x. (x) (y) d x d y + Q Ω Ω δP (x)δP (y) Ω Pst (5.20) 5.1.2 Linear Stability Analysis In order to determine the stability of stationary solutions of (5.4) by means of linear stability analysis it is helpful to require that δ 2 UNL /δP (x)δP (y) =

114


χ (x, y) satisfies the symmetry relation χ (x, y) = χ (y, x), which implies that the symmetry relation χ(x, y) = χ(y, x) holds for δ 2 F/δP (x)δP (y) = χ(x, y). Next, we linearize (5.3) at Pst . That is, we put P (x, t; u) = Pst (x) + (x, t). Using (4.17) and taking only -terms of first order into account, we obtain

∂ δ 2 F [Pst ] M (x, t) = ∇ · Pst ∇ (y, t) d y . (5.21) ∂t Ω δP (x)δP (y) Let us consider the functional L defined by the second variation of F as L[P, Pst ] =

1 2 δ F [Pst ]() , 2

(5.22)

with = P −Pst . Differentiating L with respect to t, exploiting the symmetry of δ 2 F/δP (x)δP (y), integrating by parts and assuming that the surface terms vanish, from (5.21) we obtain d d 1 2 δ F [Pst ]() L= dt 2 dt

Pst ∇ =− Ω

Ω

δ 2 F [Pst ] (y, t) dM y δP (x)δP (y)

It is clear from this result that dL/dt = 0 implies

δ 2 F [Pst ] (y, t) dM y = C , Ω δP (x)δP (y)

2 dM x ≤ 0 . (5.23)

(5.24)

where C is a constant. Multiplying (5.24) by (x, t), integrating the result with respect to x, and taking the normalization constraint Ω (x, t) dM x = 0 into account, we get d L = 0 ⇒ δ 2 F [Pst ]() = 0 . dt

(5.25)

In sum, using linear stability analysis, two fundamental results can be found [187]: the inequality (5.23) and the implication (5.25). These results can now be used to analyze the stability of stationary probability densities related to stationary (or critical) points of F . Minima Let us consider a distribution function Pst with δ 2 F [Pst ]() > 0 for all (x) = 0 and δ 2 F [Pst ]() = 0 ⇔ = 0. Then, from (5.22), (5.23), and (5.25) it follows that d d L≥0, L≤0, L=0⇔=0. (5.26) dt dt


115

Consequently, the limiting cases limt→∞ (x, t) = 0 and limt→∞ P (x, t; u) = Pst hold for all initial distributions u ≈ Pst . In other words, by means of linear stability analysis related to the second variation of free energies we reobtain the proposition (5.18). Next, we define the norm · for positive definite δ 2 F and functions (x) with Ω (x) dM x = 0 by =

δ 2 F [Pst ]() .

(5.27) 2

For details, see Sect. 5.1.8 below. Using 2L() = δ 2 F [Pst ]() = dL/dt = d /dt and (5.26), we obtain ∀ = 0 ⇒

d < 0 . dt

⇒

(5.28)

Equation (5.28) tells us that the norm of every small perturbation of Pst decreases as a function of time if Pst corresponds to a free energy minimum with δ 2 F > 0, which means once again that Pst is asymptotically stable. Maxima If Pst describes a maximum of F with δ 2 F [Pst ]() < 0 for all (x) = 0, we can introduce a norm defined by = − δ 2 F [Pst ]() , (5.29) 2

see Sect. 5.1.8. Using −2L() = −δ 2 F [Pst ]() = ⇒ −dL/dt = d /dt and (5.26), we obtain d ∀ = 0 ⇒ > 0 . (5.30) dt Equation (5.30) tells us that the norm of every small perturbation of Pst increases as a function of time if Pst corresponds to a free energy maximum with δ 2 F < 0, which means that Pst is unstable. In sum, we realize that Lyapunov’s direct method and linear stability analysis yield consistent results irrespective of the form of internal energy functionals U . From both methods it follows that stationary probability densities are asymptotically stable if they correspond to free energy minima with positive definite second variations. In contrast, if there is a perturbation of a stationary probability distribution that involves a decrease of the free energy (5.1) then the stationary distribution is (usually) an unstable one. 5.1.3 Self-Consistency Equation Analysis In Sect. (2.3) we have shown that self-consistency equations can be used to determine the stationary probability densities of nonlinear Fokker–Planck equations. Self-consistency equations can also be used to examine the stability

116


of the stationary probability densities. Let us consider the one-dimensional self-consistency equation m = R(m) . (5.31) We assume that solutions of (5.31) determine the stationary order parameter values Ast that, in turn, determine the stationary distributions Pst (x; Ast ). In this context, frequently the claim is made that the derivative of R(m) at m = Ast determines the stability of a stationary distribution. In particular, the hypothesis is made that the following implications hold: dR < 1 ⇒ Pst is asymptotically stable, dm A st dR > 1 ⇒ Pst is unstable. (5.32) dm A st

Equation (5.32) states that if the slope of R(m) at an intersection point of R(m) with the diagonal is larger than unity, we deal with an unstable stationary probability density. If the slope of R(m) at m = A is smaller than unity then we deal with an asymptotically stable stationary distribution, see Fig. 5.2. Note that there is no rigorous proof for the statements “Pst is asymptotically stable” and “Pst is unstable” in (5.32). Equation (5.32) provides us with a helpful hint that has to be verified or falsified by alternative considerations (e.g., by solving numerically the equations under consideration). Note also that we do not make any claims about stationary distributions related to dR(Ast )/dm = 1. Where does (5.32) come from? We may say that the proposition (5.32) is inspired by the theory of iterative maps [409]. Let R(z) denote a function that defines the mapping xn = R(xn−1 ) . (5.33) Equation (5.33) defines for every initial value x0 a sequence of values {x0 , x1 , . . .} and is referred to as an iterative map. The stationary points of the map (5.33) satisfy xst = R(xst ) . (5.34) Figure 5.3 shows an example of a function R(z) and the stationary points of the corresponding map. For the iterative map (5.34) one can prove that the stability of a stationary point xst is determined by the derivative of R at the point xst . A stationary point xst is asymptotically stable if |dR(xst )/dx| < 1 holds and unstable if |dR(xst )/dx| > 1 holds. Consequently, the stability criteria of the iterative map resemble those given by (5.32). Comparing the stability analysis by means of self-consistency equations and the stability analysis for iterative maps, we realize that there are two differences. First, as we have mentioned earlier, the validity of (5.32) has not yet been proven for the general case. In contrast, for iterative maps it can be proven rigorously


117

R(m)

m

Fig. 5.2. Left- and right-hand sides of a self-consistency equation. Intersection points describe stationary distributions. Self-consistency equation analysis makes the hypothesis that intersection points marked by full (empty) dots describe asymptotically stable (unstable) stationary distributions

R(z)

z

Fig. 5.3. Left- and right-hand sides of the self-consistency equation of an iterative map. Intersection points describe stationary points. Intersection points marked by full (empty) dots describe asymptotically stable (unstable) stationary points

118


that self-consistency equation analysis yields the correct results. Second, stationary points xst of iterative maps are unstable for dR(xst )/dx < −1. That is, the amount of the slope is a crucial issue here. In contrast, as we will show in Sect. 5.1.5, stationary probability densities of nonlinear Fokker–Planck equations can be stable if the inequality dR(Ast )/dm < −1 holds. It seems that the crucial issue for the stability of stationary probability densities of nonlinear Fokker–Planck equations is whether or not the slope is larger than unity. 5.1.4 Shiino’s Decomposition of Perturbations Shiino proposed to decompose perturbations of stationary probability densities into particular functions such that, on the one hand, all kinds of perturbations can be represented and, on the other hand, the decomposition can be used to determine the character of extrema of free energy measures [522, 523]. Let us illustrate Shiino’s decomposition for a perturbation (x). First, we write (x) as (x) = Pst (x) (x) , (5.35) where Pst describes a critical point (extrema) of a free energy measure. Let us proceed with three remarks concerning (5.35). First, we assume that Pst > 0 for x ∈ Ω. Therefore, (5.35) describes a one-to-one mapping between the functions (x) and (x). Consequently, if we consider (x) rather than (x), then we still take all possible perturbations into account. Second, if we examine different stationary or critical points of free energy measures then we are dealing with different stationary distributions Pst , say,Pst1 , Pst2 , and so on. Consequently, we obtain different mappings: (x) = Pst1 (x) (x), 2 (x) = Pst (x) (x), and so on. Third, the normalization condition for (x) reads Ω (x) dx = 0 and implies that

Pst (x) (x) dx = 0 . (5.36) Ω

Next, we decompose (x) into two orthogonal functions: χ0 (x) and χ⊥ (x). That is, we put (x) = χ0 (x) + χ⊥ (x) (5.37) with

χ0 (x)χ⊥ (x) dx = 0 .

(5.38)

Ω

The key idea is to relate χ0 (x) to the order parameter functions of the problem at hand, while χ⊥ (x) is used to guarantee that we still consider all possible perturbations. Let us assume that we have an order parameter A. Then, we put χ0 (x) = β[A(x) − A] Pst (x) , (5.39)


119

where β describes an amplitude. As we will show in a moment, this choice of χ0 (x) is a very useful one. From (5.39) it follows that (x) can be written as (x) = β[A(x) − A]Pst (x) + χ⊥ (x) Pst (x) . (5.40) The normalization condition Ω (x) dx = 0 implies that the integral relation

χ⊥ (x) Pst (x) dx = 0 (5.41) Ω

holds. Equations (5.38), (5.39), and (5.41), in turn, imply that χ⊥ (x) satisfies

(5.42) A(x)χ⊥ (x) Pst (x) dx = 0 . Ω

Now, let us demonstrate the power of this kind of expansion. In order to discuss the character of free energy extrema we will often be concerned with two kinds of integrals:

A(x)(x) dx , (5.43) A = Ω

2 (x) δ 2 SB [Pst ] = dx , (5.44) Ω Pst (x) where SB = BS denotes the Boltzmann entropy. Using (5.40) and (5.42), we find (5.45) A = β KA (X) . In (5.45) the variable KA (X) denotes the generalized variance defined by 2 KA (X) = A(X)2 − A(X) = [A − A]2 . (5.46) Note that by definition we have KA (X) ≥ 0. Moreover, for A(x) 2 = x the 2 variance KA (X) reduces to the conventional one: K(X) = X − X . Using (5.40-5.42), we find

δ 2 SB [Pst ] = β 2 KA (X) + χ2⊥ (x) dx . (5.47) Ω

Let us summarize. If we need to determine the character of stationary points of F by evaluating δ 2 F , then we will often deal with expressions like A

and δ 2 SB [Pst ]. If we use Shiino’s decomposition, these expressions can conveniently be expressed in terms of (5.45) and (5.47). The amplitude β measures the strength of a perturbation ∝ [A(x) − A]Pst (x). There are two extreme cases. First, we may put χ⊥ = 0 and β = 0. Then, we consider perturbations (x) = β[A(x) − A]Pst (x) .

(5.48)

120


Second, we may put χ⊥ = 0 and β = 0 and consider perturbations (x) = χ⊥ (x) Pst (x) ,

(5.49)

where χ⊥ (x) denotes an arbitrary function satisfying the constraints (5.41) and (5.42). Shiino’s decomposition can be generalized to the case that we deal with several order parameters A1 , . . . , Ad [199, 526, 527]. Then, we need to introduce several amplitudes βi , see also below. In addition, the decomposition can be generalized for free energy measures involving entropies different from the Boltzmann entropy [525, 526, 527]. 5.1.5 Generic Cases K-Model: F ∝ K A free energy Fokker–Planck equation that has frequently been studied is given by ∂ ∂ dV (x) ∂2 P (x, t; u) = + κ (x − XP ) P + Q 2 P , (5.50) ∂t ∂x dx ∂x with κ ≥ 0. We can verify that (5.50) can be written as ∂ ∂ ∂ δF P (x, t; u) = P , ∂t ∂x ∂x δP

(5.51)

with F given by

V (x)P (x) dx +

F [P ] = Ω

κ K(X) − Q BS , 2

(5.52)

2 where K denotes the variance K = X 2 − X and BS is the Boltzmann B entropy S = − Ω P ln P dx. We will refer to (5.50) as the K-model. Note that the K-model is usually discussed in the context of natural boundary conditions. That is, we have x ∈ Ω = lR. Note also that (5.51) is the univariate version of (5.3). Finally, note that for the K-model a fluctuation– dissipation theorem can be found, see Sect. 3.11. From UNL = κK/2 > 0 it follows that the nonlinear energy functional UNL is bounded from below, which implies that F is bounded from below for all potentials V for which the Boltzmann distribution of V exists (see type E in Table 4.2). Consequently, the H-theorem for free energy Fokker–Planck equations applies and we conclude that transient solutions of the K-model converge to stationary ones in the long time limit. The free energy (5.52) may alternatively be expressed as

κ F [P ] = V (x)P (x) dx + [x − y]2 P (x)P (y) dx dy − Q BS (5.53) 4 Ω Ω Ω


121

because of 2K(X) = Ω [x − y]2 P (x)P (y) dx dy. Re-arranging the terms, we obtain

κ κ [V (x)+ x2 ]P (x) dx− xyP (x)P (y) dx dy−Q BS . (5.54) F [P ] = 2 2 Ω Ω Ω In this case, comparing (5.1) and (5.54), we find U0 (x) = V (x) +

κ 2 x , 2

κ 2 UNL = − X . 2

(5.55)

As a result, (5.5) reads Pst (x) =

V (x) + κx2 /2 − κx Xst 1 , exp − Z Q

(5.56)

which can be solved by means of the corresponding self-consistency equation for the order parameter m = Xst . In line with (5.9), we define P (x, m) and R(m) by 1 V (x) + κx2 /2 − κxm P (x, m) = , exp − Z(m) Q

R(m) = xP (x, m) dx , (5.57) Ω

where Z(m) is given by Z(m) = Ω exp{−[V (x)+κx2 /2−κxm]/Q} dx. Then, Xst is given by the solutions of m = R(m). For the K-model the second variation of F reads

2 (x) δ 2 F [Pst ]() = −κ dx x (x) dx y (y) dy + Q Ω Ω Ω Pst (x)

2

2 (x) dx , (5.58) = −κ x (x) dx + Q Ω Ω Pst (x) and can be evaluated using Shiino’s decomposition (x) = β [x − Xst ] Pst (x) + χ⊥ (x) Pst (x) , (5.59) where χ⊥ satisfies the orthogonality relations Ω χ⊥ (x) Pst (x) dx = 0 and xχ⊥ (x) Pst (x) dx = 0 (see Sect. 5.1.4). Then, one obtains Ω

2 2 δ F [Pst ]() = β Kst (X) [Q − κ Kst (X)] + Q [χ⊥ ]2 dx , (5.60) Ω

where Kst (X) denotes the variance of a stationary distribution of the form (5.56). In view of (5.60) we introduce the stability coefficient ˜ = Q − κKst (X) . λ

(5.61)

122


˜ = Q − κKst (X) > 0 It can be seen now that for a distribution Pst with λ we have δ 2 F > 0 for all = 0. Consequently, from the stability analysis carried out in Sect. 5.1, we conclude that in this case Pst corresponds to a stable stationary probability density. In contrast, for every distribution Pst ˜ < 0 there exists an ∗ (namely, ∗ = β(x − X )Pst with that yields λ st χ⊥ = 0) such that δ 2 F [Pst (∗ ) < 0 and we deal with an unstable stationary distribution. Critical parameter values of κ and Q define a bifurcation line, ˜ = 0 ⇒ Q = κKst (X; κ, Q). which can be computed from λ In the preceding, we have exploited linear stability analysis and the stability analysis by means of Lyapunov’s direct method. Now, let us turn to the stability analysis by means of self-consistency equations. From (5.57) it follows that the relation dR(m) κ = K(X)P (x,m) ≥ 0 dm Q

(5.62)

holds, where the averaging is carried out with respect to P (x, m). That is, R(m) is a monotonically increasing function. In particular, we have dR κ = Kst (X) . (5.63) Q dm X st

In view of the hypothesis (5.32), we are inclined to say that stationary distributions with κKst /Q > 1 (< 1) are unstable (asymptotically stable). In fact, this is the result derived by means of Lyapunov’s direct method and linear stability analysis. Therefore, we have proven that for the K-model the proposition (5.32) made by self-consistency equation analysis is correct. Compensated B(A)-Model: F ∝ B(A) Next, we consider systems with internal energy functionals UNL [P ] = B0 (X) + B(A) ≥ Bmin and free energy measures described by

F [P ] = V (x)P (x) dx + B0 (x)P (x) dx + B(A) − Q BS[P ] , Ω

(5.64)

(5.65)

Ω

where A(x) denotes an arbitrary function. Here, we consider arbitrary phase spaces Ω (e.g., Ω = lR, or Ω = [a, b] with b > a). For F given by (5.65) the univariate free energy Fokker–Planck equation (5.51) reads 6 7 ∂ ∂2 ∂ dV (x) dB0 (x) dA(x) dB(z) P + Q P . P (x, t; u) = + + ∂t ∂x dx dx dx dz z=A ∂x2 (5.66)


123

From (5.64) we read offthat the nonlinearity B(A) is balanced by a potential B0 (x) such that Ω B0 P dx + B(A) is bounded from below. Consequently, we do not require that B(z) itself is bounded from below. If V (x) admits for a Boltzmann distribution W ∝ exp{−V /Q}, then F is a type-F free energy of Table 4.2, which implies that F is bounded from below. In this case, on account of the H-theorem for free energy Fokker–Planck equations (see Sect. 4.3), we conclude that the limiting case limt→∞ ∂P/∂t = 0 holds. Since we have δUNL [P ]/δP = B0 (x) + A(x)dB(A)/dz, (5.5) becomes V (x) + B0 + A(x)dB(Ast )/dz 1 . (5.67) Pst (x) = exp − Z Q Let us introduce the functions 1 V (x) + B0 (x) + A(x)dB(m)/dm , P (x, m) = exp − Z(m) Q

R(m) = A(x)P (x, m) dx , (5.68) Ω

where Z(m) is the normalization constant of P (x, m). Then, Ast is given by the solutions of the self-consistency equation m = R(m) .

(5.69)

Let us determine the stability of the distributions (5.67) by means of linear stability analysis and Lyapunov’s direct method. Since the second variational derivative of UNL reads δ 2 UNL [P ]/δP (x)δP (y) = A(x)A(y)d2 B(A)/dz 2 , (5.20) can be found as

2

2 (x) d2 B(z) A(x) (x) dx + Q δ F [Pst ]() = dx . dz 2 A Ω Ω Pst (x) 2

(5.70)

st

In order to evaluate (5.70), we use perturbations given by (5.71) (x) = β [A(x) − A(X)st ] Pst (x) + χ⊥ (x) Pst (x) , where the function χ⊥ (x) satisfies the constraints Ω χ⊥ (x) Pst (x) dx = 0 and Ω A(x)χ⊥ (x) Pst (x) dx = 0 (see Sect. 5.1.4). Substituting (5.71) into (5.70), one can determine the sign of δ 2 F from 7 6

2 B(z) d 2 2 + Q [χ⊥ ]2 dx , δ F [Pst ]() = β KA,st (X) Q + KA,st (X) dz 2 A Ω st

(5.72) with KA (X) defined by (5.46). For the sake of convenience, we introduce the stability coefficient

124


d2 B(z) ˜ λ = Q + KA,st (X) dz 2 A

.

(5.73)

st

˜ > 0 we obtain δ 2 F > 0 indicating that the stationary distribution For λ ˜ < 0 there is a perturbation being studied is asymptotically stable. For λ that yields δ 2 F < 0, which tells us that we are dealing with an unstable stationary distribution. The critical parameter value of Q can be computed ˜ = 0 ⇒ Q + d2 B(m)/dm2 KA,st (X) = 0 with m = A . from λ st Now, let us determine the stability of distributions satisfying (5.67) by means of self-consistency equation analysis. To this end, we define the parameter dR ˜ λ =Q 1− , (5.74) dm A st

and compute the derivative of R(m) from (5.68): dR(m) 1 d2 B(z) = − (X) K A,st dm A Q dz 2 A st

.

(5.75)

st

Based on the hypothesis (5.32) made by self-consistency equation analysis, ˜ = Q + KA,st d2 B/dz 2 > 0 (< 0) the stationary we may conclude that for λ distributions (5.67) are asymptotically stable (unstable). In fact, we have ˜ which means that self-consistency equation analysis, Lyapunov’s ˜ = λ, λ direct method, and linear stability analysis yield the same result. In other words, for the B(A)-model we have found rigorous proof that the proposition (5.32) made by self-consistency equation analysis is correct. Let us briefly address two special cases of the B(A)-model. KA -Model: F ∝ KA = κ [A − A]2 Here, we have ∂2 dA(x) ∂ ∂ dV (x) A(X)P + κ A(x) − P (x, t; u) = P + Q 2P , dx dx ∂x ∂t ∂x (5.76) and

V (x) + κA2 (x)/2 − κA(x) Ast 1 . Pst (x) = exp − Z Q

(5.77)

Transient solutions converge to stationary solutions of the form (5.77). Using 1 V (x) + κA(x)2 /2 − κA(x)m P (x, m) = , exp − Z(m) Q

R(m) = A(x)P (x, m) dx , (5.78) Ω


125

the order parameter m = Ast can be computed from m = R(m). Note that we have κ dR(m) = KA (X)|P (x,m) ≥ 0 (5.79) dm Q dR κ = KA,st (X) . dm A Q

and

(5.80)

st

˜ reads The stability coefficient λ ˜ = Q − κKA,st (X) λ and can be obtained from

(5.81)

dR ˜ =Q 1− λ . dm A

(5.82)

st

˜ > 0 (λ ˜ < 0) we have δ 2 F [Pst ] > 0 (δ 2 F [Pst ] < 0) and stationary For λ distributions are asymptotically stable (unstable). Moreover, the proposition (5.32) made by self-consistency equation analysis is correct. The free energy measure of the KA -model is reported in Table 5.1. Bounded B(A)-Model: F ∝ B(A) ≥ Bmin We consider the free energy Fokker–Planck equation 6 7 ∂ ∂ dV (x) dA(x) dB(z) ∂2 P (x, t; u) = + P + Q 2P , ∂t ∂x dx dx dz z=A ∂x

(5.83)

for B(z) ≥ Bmin . Transient solutions converge to stationary ones for t → ∞. Stationary distributions are given by V (x) + A(x)dB(Ast )/dz 1 . (5.84) Pst (x) = exp − Q Z The order parameter Ast corresponds to solutions of m = R(m) with V (x) + A(x)dB(m)/dm 1 exp − , P (x, m) = Z(m) Q

R(m) = A(x)P (x, m) dx . (5.85) Ω

The stability coefficient reads d2 B(z) ˜ λ = Q + KA,st (X) dz 2 A

(5.86) st

126


and can alternatively expressed by dR ˜ . λ=Q 1− dm A

(5.87)

st

˜ > 0 (λ ˜ < 0) we have δ 2 F [Pst ] > 0 (δ 2 F [Pst ] < 0) and stationary For λ distributions are asymptotically stable (unstable). Moreover, the proposition (5.32) made by self-consistency equation analysis is correct. For the free energy measure of the bounded B(A)-model, see Table 5.1. Summary In Table 5.1 we have summarized the four models for which we have proven above the consistence between self-consistency equation analysis, on the one hand, and Lyapunov’s direct method and linear stability analysis, on the other. In doing so, for these four models we have given rigorous proof that the proposition (5.32) made by self-consistency equation analysis is correct. For further examples, the reader is also referred to [526, 527]. Table 5.1. Generic free energy cases [187] (S = BS=Boltzmann entropy) K-model

UNL F ˜ λ

KA -model

Bounded B(A)-model

κKA κK B ≥ Bmin 2 2 κKA κK −QS V + B −QS −QS V + V + 2 2 d2 B Q − κKst Q − κKA,st Q + KA,st dm2

Compensated B(A)-model B0 + B ≥ Bmin V +B0 +B −QS Q + KA,st

d2 B dm2

5.1.6 Higher-Dimensional Nonlinearities: d > 1 d Compensated Case: UNL = i=1 κi [Ai − Ai ]2 /2 In the case of higher nonlinearities one may consider stochastic processes described by the free energy Fokker–Planck equation [526, 527] 6 7 d ∂ ∂ dV (x) ∂2 dAi P (x, t; u) = P +Q 2 P , κi Ai (x) − + Ai (X)P ∂t ∂x dx dx ∂x i=1 (5.88) which involves the free energy


F [P ] =

d κi

127

KAi (X) − Q BS[P ] ,

(5.89)

1 1 κi [Ai − Ai ]2 = κi KAi (X) . 2 i=1 2 i=1

(5.90)

V (x)P (x) dx + Ω

i=1

2

and the internal energy functional d

UNL [P ] =

d

For κi ≥ 0 and natural boundary conditions and for arbitrary κi but periodic boundary conditions, we deal with free energy functionals of the type F (or E) in Table 4.2 and, consequently, we have F ≥ Fmin and ∂P/∂t = 0 for t → ∞. If we cast (5.89) into the form 7

6 d d x2 κi 2 F [P ] = κi V (x) + P (x) dx − Ai − Q BS[P ] , (5.91) 2 2 Ω i=1 i=1 U0 (x) we obtain from (5.8) the implicit equation " d ! V (x) + i=1 κi A2i (x)/2 − κAi (x) Ai st 1 Pst (x) = exp − Z Q

,

(5.92)

which describes stationary probability densities of (5.88). In order to determine the order parameter values Ai st , we define the functions

Ai (X)P (x, m) dx , (5.93) Ri (m) = Ω

for i = 1, . . . , d involving the vector m = (m1 , . . . , md ) in combination with " d ! V (x) + i=1 κi A2i (x)/2 − κAi (x)mi 1 P (x, m) = exp − , Z(m) Q " d !

V (x) + i=1 κi A2i (x)/2 − κAi (x)mi Z(m) = dx . (5.94) exp − Q Ω Then, solutions of the self-consistency equation m = R(m) ,

(5.95)

with R = (R1 , . . . , Rd ) correspond to order parameters Ai st = mi satisfying (5.92). The second variation of (5.91) reads δ F [Pst ]() = − 2

d i=1

κi Ω

2

Ai (x) (x) dx + Q Ω

2 (x) dx . Pst (x)

(5.96)

128


Now, let us put (x) =

Pst (x) (x) and

d

(x) =

ai [Ai − Ai st ] Pst (x) + χ⊥ (x) ,

(5.97)

i=1

where χ⊥ (x) is orthogonal to the functions χi (x) defined by χi (x) = [Ai (x) − Ai st ] Pst (x). Then, χ⊥ (x) satisfies

[Ai (x) − Ai ] Pst (x)χ⊥ (x) dx = 0 , (5.98) Ω

and, on account of

(x) dx = 0, we have

χ⊥ (x) Pst (x) dx = 0 ,

Ω

(5.99)

Ω

which leads to

Ai (x)χ⊥ (x) Pst (x) dx = 0 .

(5.100)

Ω

In sum, without any loss of generality we consider perturbations (x) described by (x) =

d

ai [Ai (x) − Ai (X)st ] Pst (x) + χ⊥ (x) Pst (x) .

(5.101)

i=1

Using 2 (5.96) and exploiting the relations (5.98-5.100), we can determine /Pst dx and Ω Ai (x)(x) dx and obtain Ω

Ω

2 dx = Pst =

6 d Ω

72 ai (Ai (x) − Ai st )

i=1

d

[χ⊥ ]2 dx

Pst (x) dx + Ω

[χ⊥ ]2 dx

ai ak cik +

(5.102)

Ω

i,k=1

and

Ai (x) (x) dx = Ω

d

ak cik ,

(5.103)

k=1

where the stationary cross-correlations cik are defined by cik = cki = Ai Ak st − Ai st Ak st .

(5.104)

Note that for A(x) = x the coefficients cik reduce to the cross-correlation coefficients (Xi − Xi st )(Xk − Xk st )st . Substituting these results into (5.96) gives us

5.1 Stability Analysis d

δ 2 F [Pst ]() =

6 ai ak Qcik −

i,k=1

d

7

129

[χ⊥ ]2 dx .

κl cil ckl + Q

(5.105)

Ω

l=1

By means of the stability matrix ˜ ik = Qcik − λ

d

κl cil ckl

(5.106)

l=1

extrema of F can be classified and the stability of stationary distributions ˜ ik is positive definite then we have δF [Pst ] > 0 and can be determined. If λ Pst describes a minimum of F , which implies that Pst corresponds to an asymptotically stable stationary probability density. If there exists at least d ˜ ik < 0, then there exists at least one one vector y ∈ lRd with i,k=1 yi yK λ perturbation which yields δF [Pst ]() < 0. In this case, Pst describes a saddle-point or a maximum of F and corresponds to an unstable stationary distribution. Bounded Case: UNL [P ] = −

d i=1

κi Ai

2

In this case, we deal with the evolution equation 6 7 d ∂ dU0 (x) dAi (x) ∂2 ∂ − Ai (X)P P + Q 2 P (5.107) P (x, t; u) = κi dx dx ∂x ∂t ∂x i=1 related to the free energy measure

U0 (x)P (x) dx −

F [P ] = Ω

d κi i=1

2

2

Ai − Q BS[P ] .

(5.108)

d 2 For bounded potentials UNL [P ] = − i=1 κi Ai ≥ UNL,min we deal with free energies of type F in Table 4.2 (or E with UMF (x, y) = −κi Ai (x)Ai (y)/2). Consequently, we conclude that the relations F ≥ Fmin and limt→∞ ∂P/∂t = d 2 0 hold. For example, for κi ≥ 0 we have the inequality − i=1 κi Ai ≥ 0, ∞ which means that UNL [P ] is bounded from below. For Ai ∈ C (Ω) and systems defined on finite phase spaces Ω (e.g. systems subjected to periodic boundary conditions) the functions Ai assume minimum values on Ω and, d 2 consequently, the expression − i=1 κi Ai is bounded from below for arbitrary κi . Equation (5.107) can be treated just like the previous case when d we replace V (x) + i=1 κi A2i (x)/2 by U0 (x). Thus, we obtain d U0 (x) − i=1 κi Ai (x) Ai st 1 , (5.109) Pst (x) = exp − Z Q and

130


Ri (m) =

Ai (x)P (x, m) dx ,

(5.110)

Ω

for R = (R1 , . . . , Rd ) and m = (m1 , . . . , md ) with d U0 (x) − i=1 κi Ai (x)mi 1 , exp − P (x, m) = Q Z(m) d

U0 (x) − i=1 κi Ai (x)mi Z(m) = dx . exp − Q Ω

(5.111)

The stationary order parameter Ast in (5.109) corresponds to the solutions of the self-consistency equation m = R(m). The second variation δ 2 F of F given by (5.108) is described by (5.96). Therefore, the stability of the stationary distributions defined by (5.109) can be determined as in the previous ˜ ik defined by (5.106) is positive definite for case. Accordingly, if the matrix λ adistribution Pst , then Pst is asymptotically stable. If there exists a y with d ˜ i,k=1 yi yK λik < 0, then Pst is unstable. Special Case: Diagonal Cross-correlation Matrix Of particular interest are stochastic processes for which the cross-correlation matrix given by the coefficients cik assumes diagonal form: cik = δik cii , cii = KAi ,st (X) ≥ 0 .

(5.112)

In this case, (5.105) and (5.106) reduce to δ 2 F [Pst ]() =

d

[ai ]2 KAi ,st (X) [Q − κi KAi ,st (X)] + Q

i=1

[χ⊥ ]2 dx (5.113) Ω

and ˜i , ˜ ik = δik KA ,st (X)λ λ i

˜ i = Q − κi KA ,st (X) . λ i

(5.114)

˜ i > 0 holds for all i, then For systems of this kind we conclude that if λ we have δF [Pst ] > 0 and Pst is asymptotically stable. In contrast, if there ˜ i∗ < 0, then there exists a perturbation (x) is at least one index i∗ with λ (namely, (x) = ai∗ (Ai∗ (x) − Ai∗ st )Pst with ai = 0 for i = i∗ and χ⊥ = 0) with δF [Pst ]() < 0 and, consequently, Pst is unstable. 5.1.7 Multiplicative Noise We consider now systems subjected to multiplicative noise [298, 498]. Our objective is to analyze multiplicative noise systems by means of the methods developed in the previous section. To this end, we consider the univariate free energy Fokker–Planck equation


∂ ∂ δF ∂ , P (x, t; u) = M (x)P ∂t ∂x ∂x δP

131

(5.115)

which involves a state-dependent mobility coefficient M > 0. We assume that stationary distributions of (5.115) are defined by δF/δP = µ. Lyapunov’s Direct Method Since (5.115) corresponds to a special case of (4.49) the relations dF/dt ≤ 0 and dF/dt = 0 ⇔ ∂P/∂t = 0 hold. Using Lyapunov’s direct method, we conclude that stationary distributions Pst are asymptotically stable if the inequality ∀ = 0 : δ 2 F [Pst ]() > 0 holds. If there is at least one perturbation that yields δ 2 F [Pst ]() < 0, then we deal with an unstable stationary distribution. Linear Stability Analysis From (5.115) it follows that perturbations of stationary distributions satisfy the evolution equation

∂ ∂ ∂ δ2 F (y, t) dy . (5.116) (x, t) = M (x)Pst ∂x Ω δP (x)δP (y) ∂t ∂x Just as for systems with M = 1, we can show that if Pst is related to a free energy minimum with δ 2 F [Pst ]() > 0 for = 0, then = δ 2 F [Pst ]() decreases as a function of time and Pst is asymptotically stable. For free energy maximum distributions with δ 2 F [Pst ]() < 0 for = 0 one finds 2 that the norm = −δ F [Pst ]() increases as a function of time which means that distributions of this kind are unstable. From this discussion we see that Lyapunov’s direct method and linear stability analysis yield consistent results. Let us interpret next the state-dependent mobility coefficient M (x) in terms of a multiplicative noise source. Multiplicative Noise Sources It is clear that due to the state-dependency of M we deal with stochastic processes with multiplicative noise. However, M also occurs in the drift term. For example, for the free energy measure F = V (X) + κKA (X)/2 − Q BS (see Table 5.1, KA -model), (5.115) becomes ∂ P (x, t; u) = ∂t ∂ ∂ dA(x) ∂ dV (x) P + Q M (x) P. M (x) + κ A(x) − A(X)P ∂x dx dx ∂x ∂x (5.117)

132


Using the transformation (M, A, V ) → (D, A , V ) given by dV dM dV + κM A , =M −Q dx dx dx D(x) = QM (x) , 0 κ A(x) , A (x) = Q we can transform (5.117) into ⎡

(5.118)

⎤

2 ⎥ ∂ ∂ ⎢ ⎢ dV (x) − D(x) dA (x) A (X) ⎥ P + ∂ D(x)P . P (x, t; u) = P⎦ ∂t ∂x ⎣ dx dx ∂x2

Aeff (x,P )

(5.119) Now, let us assume that we start off with a multiplicative noise system described by means of the nonlinear Fokker–Planck equation (5.119). Then, in a first step, we transform (5.119) into (5.117) by means of the backwards transformation (D , A , V ) → (M, A, V ): 1 dV dV dD − κQA , =Q + dx dx D dx D(x) , M (x) = Q 0 Q A(x) = (5.120) A (x) . κ Since (5.117) corresponds to the free energy Fokker–Planck equation (5.115), in a second step, the stability of the stationary distributions of (5.119) can be determined using the free energy approach. That is, stationary distributions ˜ = Q − κKA,st (X) are asymptotically stable for with stability coefficients λ ˜ > 0 and unstable for λ ˜ < 0 (see Table 5.1, KA -model). In other words, from λ (5.119) it follows that multiplicative noise systems can be investigated by means of the free energy approach if the effective mean field force Aeff (x, P ) can be written as Aeff (x, P ) = D(x) A dA (x)/dx, that is, if the diffusion coefficient D(x) and Aeff (x, P ) satisfy a matching condition. 5.1.8 Norm for Perturbations∗ Let C (Ω) = f (x) | f ∈ C ∞ (Ω) ∧ Ω f (x) dM x = 0 denote the function space of the deviations of probability densities. Then the functions ∈ C are the vectors of a linear vector space and satisfy for a1 , a2 ∈ lR and 1 , 2 ∈ C

the relation a1 1 + a2 2 = 3 ∈ C . Consider a free energy functional F with second variational derivatives that are symmetric at a stationary point Pst of F,


δ 2 F [Pst ] = χ(x, y) , χ(x, y) = χ(y, x) , δP1 (x)δP2 (x)

133

(5.121)

and second variations that are positive definite at Pst : = 0 ⇔ δ 2 F [Pst ]() > 0 , = 0 ⇔ δ 2 F [Pst ]() = 0 .

(5.122)

Now, we introduce the functional

δ 2 F [Pst ] 1 (x)2 (x) dM xdM y . (5.123) (1 , 2 ) = δ 2 F [Pst ](1 , 2 ) = δP (x)δP (x) 1 2 Ω This expression is a bilinear form satisfying (1 , 2 ) = (2 , 1 ) , (a1 1 + a2 2 , 3 ) = a1 (1 , 3 ) + a2 (2 , 3 ) for a1 , a2 ∈ lR. Then, we introduce the functional · defined by = δ 2 F [Pst ]() = (, ) .

(5.124)

(5.125)

Our objective is to show that the relations ≥ 0 , = 0 ⇔ = 0 , 1 + 2 ≤ 1 + 2 , a = |a|

(5.126)

are satisfied for a ∈ lR, which means that (5.125) is a norm related to a free energy minimum. It is clear from (5.122-5.125) that the first two properties and the last property in (5.126) are satisfied. The triangle inequality can be proven in line with the proof of the triangle inequality for vectors of the Euclidean space. To this end, let us first derive the Cauchy–Schwarz inequality 1 2 ≥ (1 , 2 ) . (5.127) First, consider 2 = 0. Then, (5.127) is satisfied. Second, consider 2 = 0. Then, we have 2 > 0. Next, use A A2 A A 2 A1 2 − (1 , 2 )2 A ≥ 0 ,

(5.128)

2

= (, ), and (5.124) to obtain 2

4

2

1 2 − (1 , 2 )2 2 ≥ 0 . Since we have 2 > 0, we get

(5.129)

134

5 Free Energy Fokker–Planck Equations with Boltzmann Statistics 2

2

1 2 ≥ (1 , 2 )2 .

(5.130)

For (1 , 2 ) ≥ 0 we get from (5.130) the relation 1 2 ≥ (1 , 2 ) .

(5.131) 2

2

For (1 , 2 ) < 0 we conclude from the inequality 1 2 ≥ 0 that the relation 1 2 ≥ 0 > (1 , 2 ) (5.132) holds. In sum, (5.127) holds for 2 = 0 and 2 = 0. Consider now 2

1 + 2 = (1 + 2 , 1 + 2 ) .

(5.133)

We use (5.124) to find that 2

2

2

2

2

1 + 2 = 1 + 2(1 , 2 ) + 2 ,

(5.134)

which implies that we have 2

1 + 2 − 1 − 2 = 2(1 , 2 ) .

(5.135)

Since the Cauchy–Schwarz inequality (5.127) holds, we get 2

2

2

1 + 2 − 1 − 2 ≤ 2 1 2

(5.136)

and 2

2

2

2

1 + 2 ≤ 1 + 2 1 2 + 2 = (1 + 2 ) .

(5.137)

Since the inequalities 1 + 2 ≥ 0 and 1 + 2 ≥ 0 hold, we can derive from (5.137) the triangle inequality 1 + 2 ≤ 1 + 2

(5.138)

listed in (5.126). Finally note that by analogy one can show that (5.29) describes a norm related to a free energy maximum.

5.2 Natural Boundary Conditions We will study now examples of free energy Fokker–Planck equations that are described by ∂2 ∂ ∂ (h(x) + b(X)) P + Q 2 P P (x, t; u) = − ∂t ∂x ∂x

(5.139)

and have solutions P (x, t; u) = δ(x − X(t)) subjected to natural boundary conditions with X(t) ∈ Ω = lR. We will distinguish between models that involve linear and nonlinear functions h(x) and b(z), see Table 5.2.

5.2 Natural Boundary Conditions

135

Table 5.2. Models discussed in Sect. 5.2 Model

h

b

Type

Shimizu–Yamada model Dynamical Takatsuji model Desai–Zwanzig model Bounded B(M1 )-model

linear linear nonlinear nonlinear

linear nonlinear linear nonlinear

compensated, (5.50) compensated, (5.66) compensated, (5.66) bounded, (5.83)

5.2.1 Shimizu–Yamada Model – Stationary Solutions The Fokker–Planck equation of the Shimizu–Yamada model reads ∂ ∂ ∂2 P (x, t; u) = [γx + κ(x − X)] P + Q 2 P , ∂t ∂x ∂x

(5.140)

for κ ≥ 0 and t ≥ t0 . Transient solutions of the Shimizu–Yamada model have already been derived in Sect. 3.10. Here, we will focus on the stationary case with κ > 0. Equation (5.140) can be written as a free energy Fokker–Planck equation (5.3) with F [P ] =

γ 2 κ X + K(X) − Q BS[P ] . 2 2

(5.141)

It is clear from (5.140) that we deal with a special case of (5.50). Consequently, the implicit equation (γ + κ)x2 /2 − κx Xst 1 (5.142) Pst (x) = exp − Q Z describes stationary probability densities of (5.140). Equation (5.142) can be transformed into 0 2 κ γ+κ (γ + κ) x− Pst (x) = . (5.143) exp − Xst 2πQ 2Q κ+γ Stationary distributions of this kind exist only for γ > −κ. In order to derive the self-consistency equation of the model (5.140), we define 0 2 κ (γ + κ) γ+κ exp − m x− P (x, m) = (5.144) 2πQ 2Q κ+γ and the integral R(m) =

Ω

xP (x, m) dx which reads R(m) =

κ m. κ+γ

(5.145)

136


Since we have κ > 0 and γ > −κ the self-consistency equation m = R(m) has a unique solution given by m = 0. This implies that there is a unique solution of the implicit equation (5.143) given by Xst = 0 and 0 γ+κ (γ + κ) 2 . (5.146) Pst (x) = exp − x 2πQ 2Q Using Kst = Q/(γ + κ), (5.61) becomes ˜ = Q − κKst = γQ λ γ+κ

(5.147)

and we conclude that for γ > 0 the Gaussian distribution Pst is asymptotically stable, whereas for −κ < γ < 0 the stationary distribution is unstable. In sum, the Shimizu–Yamada model (5.140) describes stochastic processes that exhibit stable stationary distributions for γ > 0, whereas these solutions become unstable for γ ∈ (−κ, 0) and cease to exist for γ < −κ. The stability of the stationary distribution (5.146) can be illustrated by several means. Cumulants First, the evolution of the first and second cumulants M1 and K can be obtained from (5.140). To this end, we multiply the nonlinear Fokker–Planck equation (5.140) with x and x2 , respectively, integrate the result with respect to x, and integrate by parts. Assuming that the surface terms thus obtained vanish, for the mean value M1 (t) = X(t) and the variance K(t) we obtain d M1 (t) = −γM1 (t) , dt d K(t) = −2(γ + κ)K(t) + 2Q . dt

(5.148) (5.149)

We see now that for γ > 0 both cumulants are asymptotically stable and converge to M1,st = 0 and Kst = Q/(γ + κ) for t → ∞, which is in line with our observation that Pst is asymptotically stable for γ > 0. For −κ < γ < 0 the variance converges to Kst = Q/(γ + κ) in the long time limit but the stationary mean value M1,st = 0 becomes unstable indicating that Pst is unstable. In addition, for γ < −κ the variance increases exponentially. Time-Dependent Free Energy The stability of the stationary distribution (5.146) can also be illustrated by means of the free energy (5.141). For example, let us consider the timedependent behavior of the free energy (5.141) for an exact time-dependent solution of (5.140). As stated in Sect. 3.10, substituting


1 [x − x0 m(t)]2 exp − P (x, t; δ(x − x0 )) = 2K(t) 2πK(t)

137

(5.150)

into (5.140), we obtain for γ = −κ m(t) = exp{−γ(t − t0 )} , Q K(t) = [1 − e−2(γ+κ)(t−t0 ) ] . γ+κ

(5.151) (5.152)

For γ > 0 the time-dependent Gaussian distribution converges to the stationary one in the long time limit. Moreover, if we substitute (5.150-5.152) into the free energy (5.141), we obtain F (t) =

Q γ γ+κ K(t) − (1 + ln[2πK(t)]) + x20 m(t)2 . 2 2 2

(5.153)

Taking the derivative with respect to t, we get d F (t) = −Q(γ + κ)e−4(γ+κ)t − γx20 e−2γt ≤ 0 . dt

(5.154)

We realize that for γ > 0 the free energy monotonically decreases as predicted by the H-theorem of free energy Fokker–Planck equations (see Sect. 4.3). In addition, we see that the limiting case dF/dt = 0 for t → ∞ holds. Free Energy as a Potential Next, let us examine the extrema of F . If we plot F over the function space of probability densities, then we see that for γ > 0 there is a minimum at Pst given by (5.146). Unfortunately, we cannot plot F as a function of probability densities. However, we can plot F for a suitably chosen family of probability densities that is described by some parameters and plot F as a function of these parameters. For this reason, we consider now the Gaussian distributions [x − M1 ]2 1 (5.155) exp − PG (x) = √ 2K 2πK described by M1 and K. For these distributions the free energy (5.141) reads F [PG ] =

Q γ γ+κ K − (1 + ln[2πK]) + M12 . 2 2 2

(5.156)

Focusing on the M1 -dependency, F can be written as F [PG ] = F (M1 = 0) +

γ (M1 )2 2

(5.157)

and represents a parabolic function, see Fig. 5.4. For γ > 0 (< 0) there is a free energy minimum (maximum) at M1 = 0. From (5.156) we read off that

138


–1.5

γ=1

–2 F(M 1)

–2.5

–3

–1 –0.8

–0.4

γ=−1 0

0.4

0.8 1 M1

Fig. 5.4. Free energy F [PG ] as a function of M1 for Q = κ = K = 1 and γ = 1 (solid line) and γ = −1 (dashed line)

–1 γ=1

–1.5 –2 F(K) –2.5 –3

γ=−1 –3.5 0.2 0.4 0.6 0.8

1 K

1.2 1.4 1.6 1.8

2

Fig. 5.5. Free energy F [PG ] as a function of the variance K for Q = κ = 1 and M1 = 0 and γ = −1 (solid line) γ = 1 (dashed line)

the limiting cases F (K → 0) → ∞ and F (K → ∞) → ∞ hold for γ > −κ. In addition, we have dF [PG] γ+κ Q = − , (5.158) dK 2 2K which implies that there is a minimum at dF [PG ]/dK = 0 ⇒ K = Q/(γ + κ) for γ > −κ, whereas for γ < −κ the free energy F [PG ] is a monotonically decreasing function with respect to K, see Fig. 5.5. We can also plot F [PG ] in the parameter space (K, M1 ). For γ > 0 there is a unique minimum at M1 = 0 and K = Kst , see Fig. 5.6.


139

1 M1

0.5 0

0.5

1

1.5 K

2

2.5

3

–0.5 –1

Fig. 5.6. Contour lines of the free energy F [PG ] in the parameter space (K, M1 ) for Q = κ = γ = 1. There is a unique minimum at K = 1 and M1 = 0 with F = − ln(2π) = −1.83. Lines denote free energy values of F = −1.8, F = −1.5, and F = −1 (from inside to outside)

Self-Consistency Equation Analysis Finally, the stability of the stationary distribution may be illustrated by means of self-consistency equation analysis and the proposition (5.32). From (5.145) we obtain dR(0) κ . (5.159) = dm γ+κ Consequently, for −κ < γ < 0 we have dR(0)/dm > 1 indicating that we are dealing with an unstable stationary solution and for γ > 0 we have

R(m)

γ0 m

Fig. 5.7. Self-consistency equation analysis based on (5.145) and m = R(m). Solid lines: R(m) for γ > 0 and γ < 0. Dashed line: diagonal of the (m, R)-plane

140


dR(0)/dm < 1 indicating that the stationary distribution (5.144) is asymptotically stable, see Fig. 5.7. These predictions are in line with the results obtained from linear stability analysis and Lyapunov’s direct method. 5.2.2 Dynamical Takatsuji Model – Basins of Attraction Order Parameter Equation of Ising Ferromagnets The magnetization M (t) of Ising ferromagnets is often described by means of the order parameter equation d M (t) = −a1 M (t) + a2 tanh(a3 M (t)) , dt

(5.160)

with a1 , a2 , a3 > 0 [7, 18, 580]. Depending on the parameters a1 , a2 , a3 , (5.160) either exhibits a unique stationary solution Mst = 0, which describes the paramagnetic phase of Ising ferromagnets, or two stable stationary solutions with Mst = 0, which describe ferromagnetic phases that are related to spin-up and spin-down configurations. In the latter case, the stationary solution Mst = 0 exists as well but is an unstable one. Order Parameter Equation for Group Behavior In the context of human group behavior, Takatsuji [561] has studied a mean field model that shows the same bifurcation diagram as the order parameter equation (5.160). According to the model by Takatsuji, a vanishing order parameter M reflects a human population in which individual behavior dominates. That is, there is no significant collective behavior. In contrast, if M = 0 the population exhibits a collective behavior, which arises due to the mean field interactions between the individuals. In view of this interpretation of the order parameter equation (5.160), at issue is to define a stochastic process by means of a dynamical mean field model such that the random variable X(t) of the process has a mean value M1 (t) = X that satisfies (5.160). In short, we will introduce next in a top-down fashion a mean field model that yields the order parameter equation (5.160). A bottom-up approach to this model can be found in Sect. 5.5.5. Dynamical Takatsuji Model Let us describe the state of a single subsystem of a many-body system by means of the random variable X(t) ∈ Ω = lR. In line with mean field theory, we assume that the single subsystem free energy reads F [P ] =

γ + c 2 X + B(X) − Q BS[P ] , 2

(5.161)


with

√ B(z) = − ln cosh( c z) .

141

(5.162)

Substituting the free energy (5.161) into (5.3), we obtain the free energy Fokker–Planck equation " √ √ ∂ ! ∂ ∂2 P (x, t; u) = (γ + c)x − c tanh( c X) P + Q 2 P . ∂t ∂x ∂x

(5.163)

The nonlinearity√B(z) satisfies B(0) = 0 and describes a parabola for small z 2 because of cosh( c z) ≈ 1 + cz 2 /2 and B(z) √ ≈ −cz /2 for z ≈ 0. For large |z| the function B(z) behaves like B(z) = − c|z| and is linear with respect to |z|. In addition, one can show that the inequality ln cosh(z ) < [z ]2 /2 holds for z = 0, which implies that −B(z) < cz 2 /2 holds for z = 0 and c > 0, see also Fig. 5.8.

12 10 8 -B(z)

6 4 2

–4

–2

0

2

z

4

Fig. 5.8. −B(z) (solid line) and c z 2 /2 (dotted line) as a function of z for c = 1.

For γ > −c the free energy is bounded from below. To see this we write F as γ + c 2 γ + c γ+c 2 X + F [P ] = K+ X + B(X) − Q BS[P ] . (5.164) 4 4 4 Since B(z) ∝ −|z| for large |z|, the expression Y = (γ + c)z 2 /4 + B(z) is bounded from below for γ > −c, which implies that the nonlinear functional 2 UNL = (γ + c)K/4 + (γ + c) X /4 + B(X) is bounded from below, whereas the linear part UL [P ] = U0 with U0 = (γ + c)x2 /4 yields a Boltzmann distribution W ∝ exp{−U0 (x)/Q}. In sum, the free energy (5.161) corresponds to a measure of type F in Table 4.2. Since F is bounded from below the Htheorem for free energy Fokker–Planck equations applies, which means that we have limt→∞ ∂P (x, t; u)/∂t = 0. Furthermore, the first moment of the solutions P (x, t; u) satisfies √ √ dVM d M1 = −(γ + c)M1 + c tanh( cM1 ) = − , dM1 dt

(5.165)

142


where V is defined by VM (z) =

√ γ 2 c 2 z + z − ln cosh( cz) . 2 2

(5.166)

Vc (z) Equation (5.165) corresponds to the √ order parameter √equation (5.160) of the Ising model for a1 = γ + c, a2 = c, and a3 = c. The potential Vc (z) vanishes at z = 0 and increases monotonically with |z| both for z > 0 and z < 0. Consequently, the potential VM (z) is monostable for γ > 0 and bistable for γ < 0 (and γ > −c, see below), see Fig. 5.9. That is, for γ ∈ (−c, 0) the potential VM describes a double-well potential and there are multiple stationary solutions of M1 .

V(z)

1

0.8 0.6 0.4 0.2 –4

–2

0 –0.2

2

4 z

–0.4

Fig. 5.9. VM (z) given by (5.166) for c = 1 and several values of the parameter γ: γ = 0.5 (dotted line) and γ = −0.5 (solid line)

Equation (5.163) corresponds to the generic free energy Fokker–Planck equation (5.66) for V (x) = γx2 /2, B0 (x) = cx2 /2, B(z) given by (5.162), and A(x) = x. Consequently, stationary solutions satisfy the implicit equation 0 2 √ √ (γ + c) γ+c c exp − tanh( c Xst ) x− Pst (x) = 2πQ 2Q c+γ (5.167) (hint: use (5.67) and determine the quadratic complement). Equation (5.68) now reads 0 2 √ 1 (γ + c) γ+c exp − tanh( c m) x− , (5.168) P (x, m) = 2πQ 2Q c+γ which implies that R(m) =

Ω

xP (x, m) dx is given by


143

√

R(m) =

√ c tanh( c m) c+γ

(5.169)

(see also (5.165) for the stationary case). Let us determine now the stationary order parameter values Xst from the self-consistency equation Xst = R(Xst ). It is clear that R(0) = 0 holds and, consequently, a stationary solution of the dynamical Takatsuji model is described by 0 γ+c (γ + c)x2 . (5.170) Pst (x) = exp − 2Q 2πQ In view of the antisymmetry property R(m) = −R(−m), we conclude that if m = 0 is a solution of the self-consistency equation m = R(m) then −m corresponds to a solution as well. Now, let us discuss under which conditions the self-consistency equation has nonvanishing solutions. First, we note that R(m) is a monotonically increasing function with " √ dR(m) c ! = 1 − tanh2 ( c m) ≥ 0 dm c+γ

(5.171)

because we have 1 − [tanh(z)]2 ≥ 0. It is clear that if dR/dm < 1 holds for all m, then m = R(m) is only solved by m = 0. The reason for this is that if R(m) with R(0) = 0 is smaller than m for m > 0 and larger than m for m < 0, then m = R(m) is only solved by m = 0. Since 0 ≤ 1 − tanh2 (z ) ≤ 1 for z ∈ lR, for γ > 0 we have ∀m : dR/dm < 1 and the self-consistency equation has a unique solution given by m = 0. In contrast, for −c < γ < 0 we have dR(0)/dm = c/(c + γ) > 1 and we find that the self-consistency equation exhibits solutions with m = 0, see Fig. 5.10.

3 2

γ0

1 –3

–2

–1

1

2

m

3

–1 –2 –3

Fig. 5.10. Illustration of the self-consistency equation m = R(m) with R(m) given by (5.169). Solid lines: R(m) for c = 1 and γ = −0.5 and γ > 0.5. Dashed line: c 2004, with permission from diagonal of the (m, R)-plane; reprinted from [182], Elsevier

144


6

(stable)

M1 4 2 (stable)

(unstable)

–1

–0.5

0.5 –2

1

1.5

γ

–4 (stable)

–6

Fig. 5.11. Bifurcation diagram for the order parameter M1 = Xst of the Takatsuji c 2004, with permission from Elsevier model (5.163); reprinted from [182],

Since we are dealing with a special case of the compensated B(A)model, the stability of stationary distributions can be determined by means of the slopes of R(m) at intersection points m = Xst . For γ > 0 we have dR(0)/dm = c/(c + γ), which implies that the stationary probability density (5.170) is asymptotically stable (because of dR(0)/dm < 1), whereas for γ < 0 the distribution (5.170) becomes unstable (because of dR(0)/dm > 1 for γ < 0). Moreover, from Fig. 5.10 we read off that for −c < γ < 0 we have dR(m)/dm < 1 at solutions m = 0 of m = R(m). Consequently, the stationary probability densities given by (5.167) with Xst = 0 are asymptotically stable if they exist. The mean values M1,st = m computed from m = R(m) for several values of γ are shown in Fig. 5.11. For γ ↓ −c the stationary mean values M1,st = 0 behave like M1,st → ±∞. For γ ≤ −c stationary solutions cease to exist. Autocorrelation Function X(t)X(t ) Our aim now is to discuss the evolution of the autocorrelation function C(t, t ) = X(t)X(t ) defined for t ≥ t ≥ t0 . From (5.165) it follows that for every initial distribution u(x) the first moment M1 corresponds to a continuous function of time: M1 = M1 (t; u). Therefore, (5.163) can equivalently be expressed as " √ √ ∂ ∂2 ∂ ! (γ + c)x − c tanh( cM1 (t; u)) P + Q 2 P (5.172) P (x, t; u) = ∂t ∂x ∂x √ √ involving the drift coefficient D1 (x, t; u) = −(γ + c)x + c tanh( cM1 (t; u)). Since D1 can be regarded as the first Kramers–Moyal coefficient of a Markov diffusion process, (5.163) is a strongly nonlinear Fokker–Planck equation and the transition probability density of the Markov diffusion process satisfies


145

2 √ √ ∂ 1 ∂ (γ + c)x − c tanh( c XP (x,t;u) ) P (x, t|x , t ; u) P (x, t|x , t ; u) = ∂t ∂x ∂2 (5.173) +Q 2 P (x, t|x , t ; u) . ∂x Multiplying (5.173) with P (x , t ; u), we obtain 2 √ √ ∂ ∂ 1 (γ + c)x − c tanh( c XP (x,t;u) ) P (x, t; x , t ; u) P (x, t; x , t ; u) = ∂x ∂t ∂2 (5.174) +Q 2 P (x, t; x , t ; u) . ∂x Multiplying this evolution equation with x and x and integrating with respect to x and x , we obtain (with the help of partial integration) the evolution equation √ √ ∂ C(t, t ) = −(γ + c)C(t, t ) + cM1 (t ) tanh( cM1 (t)) , (5.175) ∂t which 2 has to be solved under the initial condition C(t , t ) = M2 (t ) = X (t ) . Thus, we get C(t, t ) = M2 (t ) exp{−(γ + c)(t − t )}

t √ √ exp{−(γ + c)(t − z)} tanh( cM1 (z)) dz . + cM1 (t ) t

(5.176) We need to determine now the unknown second moment M2 . From (5.163) it follows that √ √ d M2 (t) = −2(γ + c)M2 (t) + 2Q + 2 cM1 (t) tanh( cM1 (t)) . (5.177) dt Note that in the stationary case this equation reduces to M2,st = Q/(γ + c) − 2 , which again gives us the variance Kst = Q/(γ + c) of the stationary M1,st distribution (5.167). In sum, solving the evolution equations for M1 (t) and M2 (t) given by (5.165) and (5.177) and substituting the result into (5.176), we can obtain for all pairs (t, t ) the autocorrelation function C(t, t ), see Fig. 5.12. Now let us show that the autocorrelation function C(t, t ) depends only on the time difference t−t in the stationary case (i.e., it becomes stationary): limt→∞,t →∞ C(t, t ) = Cst (t − t ). To this end, let us first note that if z ∈ [t , t], t ≥ t , and t → ∞ holds then we conclude that z → ∞. Consequently, t √ √ the integral in (5.176) becomes cM1,st tanh( cM1,st ) t exp{−(γ + c)(t − √ √ z)} dz. If we use c tanh( cM1,st ) = (γ + c)M1,st (see 5.165)), we obtain 2 lim C(t, t ) = M1,st + Kst exp{−(γ + c)(t − t )} = Cst (t − t ) .

t →∞

(5.178)

That is, C(t, t ) indeed becomes stationary in the stationary case. Furthermore, Cst (z) satisfies the special cases Cst (0) = M2,st and limz→∞ Cst (z) = 2 , see also Fig. 5.13. M1,st

146


8 M2

6 4

C

2 0

2

4

–2

t

6

8

10

M1

Fig. 5.12. M1 (t), M2 (t), and C(t, t ) = X(t)X(t ) as functions of t for a stochastic processes with u(x) = δ(x − x0 ). Solid lines represent results obtained from the Fokker–Planck approach, see (5.165), (5.176), and (5.177). Diamonds represent results obtained from a simulation of the Langevin equation (5.179). using the averaging method for self-consistent Langevin equations. The function X(t)X(t ) is given for t ≥ t . For t < t we have put X(t)X(t ) = 0. Parameters: Q = 1, x0 = −3, γ = −0.5, c = 1, and t = 2, t0 = 0 (L = 105 , ∆t = 0.01, wn via c 2004, with permission from Elsevier Box–Muller); reprinted from [182], 8 M2

6

C

4 2 0 –2

2

4

6

8

10 12 14 16 18 20 t M1

Fig. 5.13. As in Fig. 5.12 but for t = 12. As shown by the first and second moments 2 in this case we are in the stationary regime. The thin horizontal line describes M1,st ; c 2004, with permission from Elsevier reprinted from [182],

Basins of Attraction In case of the dynamical Takatsuji model the basins of attraction for stationary solutions can be determined. The reason for this is that for the unknown order parameter Xst occurring in the stationary distributions of the dynamical Takatsuji model, we have with (5.165) a closed evolution equation for M1 (t) = X at hand that determines Xst for every initial distribution u(x) (see also Sect. 2.4). As mentioned earlier the potential VM (z) given by (5.166) is bounded from below for γ > −c. It is monostable for γ ≥ 0 and bistable for −c < γ < 0, see Fig. 5.9. For −c < γ < 0 we conclude from (5.165) that probability densities P (x, t; u) with M1 (0) > 0 converge to the asymptotically stable, asymmetric stationary distribution (5.167) with M1,st > 0, whereas P (x, t; u) with M1 (0) < 0 converge to (5.167) with M1,st < 0, see Fig. 5.14.


147

Probability densities P (x, t; u) with a vanishing first moment converge to the unstable symmetric solution (5.170). Consequently, in the function space of probability densities the distributions u(x) with Ω xu(x) dx = 0 describe some kind of separatrix. We would like to point out that not only do all distribution functions P (x, t; u) with Ω xu(x) dx = 0 converge to the stationary distribution (5.167) with M1,st > 0 or M1,st < 0, but also all stochastic processes described by (5.163) and (5.173) and the Markov hierarchy (3.18) converge to only two kinds of stationary stochastic processes exhibiting either M1,st > 0 or M1,st < 0.

3 2 M1 1 0

2

4

6

8

t

10

–1 –2 –3

Fig. 5.14. M1 (t) as a function of t as obtained from a simulation of (5.179) (diamonds) and from solving numerically (5.165) (solid lines) for delta distributions u(x) and different M1 (0) (t0 = 0). For distributions with M1 (0) > 0 (< 0) the stochastic processes converge to the positive (negative) solution of √ √ (γ + c)M1,st = c tanh( cM1,st ) given for our parameter values by M1,st ≈ 2 (−2). Initial values: M1 (0) = 3, M1 (0) = 0.2, M1 (0) = −0.2, and M1 (0) = −3 (from top to bottom). Parameters: Q = 1, c = 1, γ = −0.5 (L = 105 , ∆t = 0.01, wn c 2004, with permission from Elsevier via Box–Muller); reprinted from [182],

Langevin Equation The Langevin equation that corresponds to the strongly nonlinear Fokker– Planck equation given by (5.163) and (5.173) reads √ √ d X(t) = −(γ + c)X + c tanh( c X) + QΓ (t) . dt

(5.179)

We can now compute the autocorrelation function C(t, t ) from (5.165), (5.176), and (5.177) obtained from the Fokker–Planck description or alternatively from the Langevin equation (5.179). As shown in Figs. 5.12 and 5.13 both methods yield the same results. In particular, Fig. 5.13 illustrates the convergence of the stationary autocorrelation function Cst (∆t) to the limit 2 value M1,st in the limit ∆t → ∞. In order to illustrate the basins of attraction, we solved the Langevin equation (5.179) for several initial values

148


of M1 . Again, we solved also the corresponding evolution equation (5.165) obtained from the Fokker–Planck description and found consistent results, see Fig. 5.14. 5.2.3 Desai–Zwanzig Model The K-model (5.50) has been studied in detail for V (x) = −ax/2 + bx4 /4 by Kometani and Shimizu [352] and Desai and Zwanzig [135]. This model is explicitly given by " ∂ ∂2 ∂ ! P (x, t; u) = − ax − bx3 − κ(x − X) P + Q 2 P , ∂t ∂x ∂x

(5.180)

for κ ≥ 0, a ≥ 0, b ≥ 0, and t ≥ t0 and is often referred to as the Desai– Zwanzig model. For κ = 0 we deal with a linear Fokker–Planck equation. For b = 0 the model (5.180) reduces to the Shimizu–Yamada model discussed in Sect. 5.2.1. In what follows, we consider the case κ > 0 and b > 0. First of all, we note that by means of the variable transformations t = at and x = x b/a and the operator relations 0 b ∂ ∂ ∂2 b ∂2 ∂ ∂ = , = , (5.181) =a , ∂t ∂t ∂x a ∂x ∂x2 a ∂x 2 we can write (5.180) as 2 2 ∂ ∂ 1 3 ∂ x P (x , t ) = − − x − κ (x − X ) P + Q P , ∂t ∂x ∂x 2 with κ = κ/a and Q = Qb/a2 for the probability density 0 0 a a t P x , ;u . P (x , t ) = b b a

(5.182)

(5.183)

Consequently, we will primarily examine solutions of (5.180) for a = b = 1. Equation (5.180) can be written as the free energy Fokker–Planck equation (5.3) with F given by [128, 523]

κ F [P ] = V (x) dx + K(X) − Q BS[P ] , 2 Ω b a (5.184) V (x) = − x2 + x4 . 2 4 The free energy corresponds to a measure of type E in Table 4.2, which implies that we have F ≥ Fmin and limt→∞ ∂P/∂t = 0. The free energy F can equivalently be expressed as

κ 2 F [P ] = U0 (x) dx − X − Q BS[P ] , 2 Ω a−κ 2 b 4 x + x . (5.185) U0 (x) = − 2 4


149

The effective potential U0 corresponds to a double-well potential for a > κ and a potential with a single minimum for a < κ, see Fig. 5.15. a κ

0.4 0.2

–2

0

–1

1

x

2

–0.2 –0.4

Fig. 5.15. Potential U0 (x) defined by (5.185) for a = b = 1, Q = 0.1 and two values of κ: κ = 0.1 and κ = 1.5

aκ

0.2

–2

–1

0

1

x

2

Fig. 5.16. Symmetric stationary solutions (5.188) of the Desai–Zwanzig model for different values of κ. Parameters correspond to those used in Fig. 5.15

Substituting V (x) = −ax2 /2 + bx4 /4 into (5.56) and (5.57), we obtain ! " bx4 /4 − (a − κ)x2 /2 − κx Xst 1 (5.186) Pst (x) = exp − Q Z and

! " bx4 /4 − (a − κ)x2 /2 − κxm 1 P (x, m) = , exp − Z(m) Q ! "

bx4 /4 − (a − κ)x2 /2 − κxm Z(m) = dx , (5.187) exp − Q Ω

150


as well as the self-consistency equation m = R(m) with R(m) = Ω xP (x, m) dx. From (5.187) it is clear that Z(0) > 0 and R(0) = 0, which implies that m = 0 is a solution of m = R(m) and ! " bx4 /4 − (a − κ)x2 /2 1 (5.188) Pst (x) = exp − Q Z describes a stationary probability density of (5.180). We refer to (5.180) as the symmetric stationary solution of the Desai–Zwanzig model. There are two types of symmetric solutions. As shown in Fig. 5.16, for κ < a we obtain an unimodal distribution, whereas for κ > a we have a bimodal distribution. Stationary mean values Xst = 0 satisfying (5.186) can be computed from m = R(m).

1.5 1

κ>κc

R(m)

κ κc

Since R(m) is an antisymmetric function (i.e, we have R(m) = −R(−m)), every solution m = 0 of m = R(m) gives us another solution of m = R(m), which is −m. The stationary probability densities (5.186) with Xst = m = 0 describe asymmetric functions (i.e., we have Pst (x) = Pst (−x)). The function R(m) increases monotonically (see (5.62)) and is shown in Fig. 5.17 for two typical cases. From Fig. 5.17 we read off that if there are solutions of m = R(m) with m = 0, then the slope of R(m) at m = 0 is larger than unity; – if there are solutions of m = R(m) with m = 0, then the slope of R(m) at these solutions is smaller than unity. –

˜ = Q − κKst (X) = Q(1 − dR(0)/dm) is positive if there Consequently, λ is only one solution of the self-consistency equation and negative if there are multiple solutions. This implies that the symmetric stationary solution (5.188) corresponds to an asymptotically stable stationary solution if it is


151

2.5

κ

2

bi

bl

sta

e

1.5 k

sta no

1

bl

e

o m 0.5 0

0.2

0.4

0.8

0.6

1 Q

Fig. 5.18. Solid line: bifurcation line in the parameter space described by κ and Q for a = b = 1. The bifurcation line separates a monostable and a bistable region. Dashed line: for κ > 1 (κ < 1) the symmetric solution (5.188) is unimodal (bimodal), see Fig. 5.16 (stable)

0.8 0.6 M1

0.4 0.2

0 –0.2

(unstable)

(stable)

0.1

0.2

g

0.3

0.4

–0.4 –0.6

0.5

κ (stable)

–0.8

Fig. 5.19. Bifurcation diagram: M1 = Xst as a function of κ for a = b = 1 and Q = 0.1 (stable)

1

M 1 0.5 (unstable)

0

0.2

(stable)

0.4

0.6

0.8

1

1.2 Q

–0.5 (stable)

–1

Fig. 5.20. Bifurcation diagram: M1 = Xst as a function of Q for a = b = 1 and κ = 2.0

152


the only solution of the implicit equation (5.186). In contrast, the symmetric solution corresponds to an unstable solution if there are asymmetric solutions satisfying (5.186). In the latter case, these additional asymmetric solutions are stable distribution functions. The critical parameter values at which the symmetric solution (5.188) ˜ = becomes unstable and multiple solutions occur can be computed from λ 0 ⇒ dR(0)/dm = 1 ⇒ Q = κK(X)Pst,m=0 , which leads to (5.189) Q = κ X 2 Pst,m=0 , where Pst,m=0 is defined by (5.188). The function κ(Q) thus obtained is shown in Fig. 5.18. Below the bifurcation line the system is monostable and exhibits a unique, symmetric, and asymptotically stable stationary probability density. Above the bifurcation line the system is bistable and exhibits two asymmetric and asymptotically stable stationary probability densities. Note also that for large Q it can be shown that the bifurcation line is described by κ = 3Q [135]. Finally, the self-consistency equation m = R(m) can be solved numerically and bifurcation diagrams can be obtained. The order parameter Xst as a function of κ and Q is shown in Figs. 5.19 and 5.20. 5.2.4 Bounded B(M1 )-Model We examine now solutions of (5.83) for A(x) = x and b(z) = −dB/dz [164]. That is, we study solutions of ∂ ∂ dU0 (x) ∂2 P (x, t; u) = − b(X) P + Q 2 P (5.190) ∂t ∂x dx ∂x that describe the evolution of systems with free energy measures given by

U0 (x)P (x) dx + B(X) − Q BS[P ] . (5.191) F [P ] = Ω

We require that the potentials U0 ∈ C ∞ (Ω) and B ∈ C ∞ (lR) are bounded from below: U0 (z) ≥ Umin and B(z) ≥ Bmin . Then, F is bounded from below (see type F in Table 4.2) and transient solutions converge to stationary ones in the long time limit (H-theorem, see Sect. 4.3). In order to describe stationary solutions of (5.190), we substitute A(x) = x into (5.84), which yields U0 (x) − xb(Xst ) 1 . (5.192) Pst (x) = exp − Z Q Likewise, (5.85) becomes 1 U0 (x) − xb(m) P (x, m) = exp − , Z(m) Q

U0 (x) − xb(m) Z(m) = dx . exp − Q Ω

(5.193)


153

Then, R(m) is defined with the help of (5.193) by R(m) = Ω xP (x, m) dx and the mean values Xst of (5.192) can be determined by means of the self-consistency equation m = R(m). Since we deal with a special case of the bounded B(A)-model, the stability of the stationary distributions (5.192) is ˜ given by λ ˜ = Q + Kst (X)d2 B(X )/dm2 (see determined by the sign of λ st (5.73) for A(x) = x). Since we have dR(m) d2 B(m) db(m) 1 1 = K(X)P (x,m) = − K(X)P (x,m) , dm Q dm2 Q dm

(5.194)

˜ can equivalently be expressed as λ ˜ = Q(1 − dR(m)/dm) the coefficient λ with m = Xst (equivalence between self-consistency equation analysis and Lyapunov’s direct method). Existence of stationary solutions Let us show now that there is at least one stationary solution of (5.190). For infinitely differentiable functions B and U0 it is reasonable to assume that R(m) is a continuous function with respect to m. Then, our objective is to show that R(m) is bounded from above for m > 0 and bounded from below for m < 0, which implies that there is at least one intersection point of R(m) and the diagonal of the (m, R)-plane (i.e., there is at least one m solving m = R(m)). Proof∗ In order to prove the aforementioned kind of boundedness, we assume that the Boltzmann distribution 1 U0 (x) (5.195) W (x) = exp − ZB Q exists (where ZB is a normalization constant ZB = Ω exp{−U0 /Q} dx) and that B(z) is globally attractive in the sense that it exhibits the asymptotic behavior B(z → ±∞) → ∞. Next, we realize that the mean of the distribution exp {−[U0 (x) − xb]/Q} dx (5.196) Pb (x) = exp {−[U0 (x) − xb]/Q} Ω is smaller than or equal to the mean of W (x) for parameter values b ≤ 0 and larger than or equal to the mean of W (x) for parameter values b ≥ 0:

xPb≤0 (x) dx ≤ XW ≤ xPb≥0 (x) dx . (5.197) Ω

Ω

The reason for this is that for b = 0 we have b ∈ lR the derivative

Ω

Pb (x) dx = XW and for

154


d db

xPb (x) dx = Ω

1 K(X)Pb ≥ 0 Q

(5.198)

is positive, which implies that Ω xPb (x) dx is a monotonically increasing function with respect to b. Next, we note that from the asymptotic behavior B(z → ±∞) → ∞ of B(z) it follows that for z → ∞ we have b(z) < 0 and P (x, m) corresponds to a distribution Pb with b(m) ≤ 0: P (x, m) = Pb(m)≤0 (x). Likewise, in the limit z → −∞ we have b(z) > 0 and P limm→∞ R(m) = (x, m) = Pb(m)≥0 (x). Consequently, the limiting cases and lim R(m) = xPb(m)≥0 (x) dx ≥ xP (x) dx ≤ X m→−∞ b(m)≤0 W Ω Ω XW hold. That is, R(m) is bounded from above for m → ∞ and from below for m → −∞. Since R(m) is assumed to be a continuous function, we conclude that R(m) is bounded from above for m > 0 and from below for m < 0. That is, we have proven the claim made above. Example Let us illustrate this issue by a more explicit example. We consider the potential γ U0 (x) = x2 (5.199) 2 with γ > 0 for which (5.192) can be written as 0 γ[x − γ −1 b(Xst )]2 γ . (5.200) Pst (x) = exp − 2πQ 2Q In addition, we consider a double-well potential B(z) = −

z4 z2 + 2 4

(5.201)

leading to b(z) = z − z 3 . Since the variance of the stationary distributions (5.200) is given by Kst (X) = Q/γ, the function 0

γ γ (x − γ −1 b(m))2 dx (5.202) x exp − R(m) = 2πQ Ω 2Q reads R(m) = b(m)/γ = (m − m3 )/γ and the self-consistency equation m = √ R(m) is solved by m = 0 for γ > 0 and m = ± 1 − γ for γ ∈ (0, 1), which means that the critical value of γ is γc = 1. Furthermore, we have dR(m)/dm = (1 − 3m2 )/γ. From this it follows that dR(m) > 1 (< 1) for γ ∈ (0, 1) (γ > 1) , dm X =0 st dR(m) > 1 for γ ∈ (0, 1) . (5.203) dm X =±√1−γ st

5.3 Periodic Boundary Conditions

155

As a result, we obtain the self-consistency equations illustrated in Fig. 5.21 and the bifurcation diagram depicted in Fig. 5.22. For γ → 0 the variance of the distribution (5.200) increases like Kst → ∞, which is in line with the fact that for γ < 0 Gaussian distributions of the form (5.200) no longer exist. Finally, note that in this example we have XW = 0 and, consequently, the limiting cases R(m) < 0 for m → ∞ and R(m) > 0 for m → −∞ hold, see also Fig. 5.21.

γγ

–0.5

0.5

c

m

1

–0.5 –1

Fig. 5.21. Illustration of the self-consistency equation m = R(m) with R(m) = (m − m3 )/γ. Solid lines: R(m) for two values of γ: γ = 0.5 < γc and γ = 1.5 > γc with γc = 1

(stable)

1

M1 0.5 (unstable)

0

0.2

(stable)

0.4

0.6

0.8 g

1

1.2

1.4

γ

–0.5 (stable)

–1

Fig. 5.22. Bifurcation diagram of the order parameter M1 for the B(M1 )-model (5.190) with U0 and B given by (5.199) and (5.201)

5.3 Periodic Boundary Conditions In this section we will discuss stochastic processes described by periodic random variables defined on Ω = [0, 2π]. We will examine the Kuramoto–

156


Shinomoto–Sakaguchi (KSS) model and the mean field Haken–Kelso–Bunz (HKB) model. Before we discuss these models, we will introduce two helpful statistical measures: the cluster amplitude and the cluster phase. 5.3.1 Cluster Amplitude and Cluster Phase The cluster amplitude r and the cluster phase θ of a 2π-periodic probability density P are defined by [365]

iX iθ re = e exp{ix}P (x) dx . (5.204) = Ω

Equation (5.204) can alternatively be written as r cos θ = cos(X) , and

r sin θ = sin(X) .

2 2 cos(X) + sin(X) = |exp{iX}| ≥ 0 , sin(X) . θ = arctan cos(X)

(5.205)

r=

(5.206)

Note that r = | exp{iX} | is not equivalent to | exp{iX}|, which is equal to unity. The cluster amplitude r satisfies P (x) = δ(x − x0 ) ⇒ r = 1 , P (x) ∈ C 0 (Ω) ⇒ r < 1 .

(5.207)

That is, for continuous distributions P (x) the cluster amplitude is smaller than unity. If P (x) corresponds to a delta distribution, then r equals unity. Moreover, for uniformly distributed random variables in the interval [0, 2π] we obtain 1 ⇒r=0. (5.208) P (x) = 2π In Fig. 5.23 realizations X k of a unimodal distribution P (x) are plotted on the unit circle. As shown in Fig. 5.23, roughly speaking, the cluster phase describes in which direction the realizations point on the average, whereas the cluster amplitude describes the degree of uniformity of the distribution and tells us how pronounced the peak of the distribution is. Similar to (5.204), one can define generalized cluster amplitudes rn and cluster phases θn [116, 117, 118, 119, 568]:

2π rn exp{inθn } = exp{inx}P (x) dx . (5.209) 0 2

2

The amplitudes rn satisfy 0 ≤ rn ≤ 1 with rn2 = cos(nX) +sin(nX) . We have rn = 0 for all n if and only if P corresponds to the uniform distribution.


157

90°

e

litud

amp

phase 0°

Fig. 5.23. Interpretation of the cluster amplitude and cluster phase. Dots represent realizations X k of a 2π-periodic random variable X

5.3.2 Kuramoto–Shinomoto–Sakaguchi (KSS) Model – Cluster Amplitude Dynamics The nonlinear Fokker–Planck equation

dUMF (x − x ) ∂ ∂2 ∂ P (x, t; u) = P (x , t; u) dx P + Q 2 P ∂t ∂x Ω dx ∂x

(5.210)

has been introduced in works by Kuramoto, Shinomoto and Sakaguchi [364, 365, 366, 506, 531, 530] and since then has extensively been studied (see Sect. 7.5). Solutions of (5.210) are subjected to periodic boundary conditions. We assume that the mean field potential satisfies the relations UMF (0) = 0 and UMF (z) = UMF (z + 2π). We will refer to (5.210) as the KSS model. Irrespective of the explicit form of UMF (z), the uniform probability density is a stationary solution of (5.210): Pst (x) =

1 . 2π

(5.211)

This can be shown by substituting (5.211) into (5.210) and taking into account that Ω UMF (x − x ) dx = 0, which is due to the fact that UMF (z) can be written as (7.149). In general, stationary probability densities of (5.210) satisfy

dUMF (x − x ) ∂ (5.212) J =− Pst (x ) dx Pst (x) − Q Pst (x) , dx ∂x Ω where J = constant and Pst (x) = Pst (x + 2π), see (2.23). Equation (5.212) is solved by J = 0 and U (x − x )Pst (x ) dx Ω MF 1 − Q Pst (x) = e . (5.213) Z

158


Free Energy Case We assume now that UMF is a symmetric function: UMF (z) = UMF (−z). The mean field potential can then be expanded into a Fourier series given by UMF (z) = −

∞

cn cos(nz)

(5.214)

n=1

and cos(n(x − x )) = cos(nx) cos(nx ) + sin(nx) sin(nx ) .

(5.215)

We have chosen a minus sign in (5.214) because in this case for cn > 0 the potential UMF (z) has a minimum at z = 0. We will refer to the evolution equation (5.210) with the potential (5.214) as the free energy case of the KSS model (or the free energy KSS model). For UMF given by (5.214) the nonlinear Fokker–Planck equation (5.210) can be written as a free energy Fokker–Planck equation (5.3) with

1 F [P ] = UMF (x − x )P (x)P (x ) dx dx − Q BS[P ] . (5.216) 2 Ω Alternatively, F can be written as ∞ 2 1 1 2 2 F [P ] = − cn cos(nX) + sin(nX) − QBS[P ] . 2 n=1

(5.217)

Stationary solutions are given by ∞

Pst (x) =

1 e Z

n=1

[cn cos(nx) cos(nX)st + cn sin(nx) sin(nX)st ] Q

(5.218)

and by the uniform distribution (5.211). Note that the uniform distribution Pst (x) = 1/(2π) can also be regarded as a solution of (5.218) because we have cos(nX) = sin(nX) = 0 for all n if the averaging is carried out with respect to the uniform distribution. Since the free energy (5.216) corresponds to a measure of type E in Table 4.2, we have F ≥ Fmin and the H-theorem discussed in Sect. 4.3 applies. That is, the limiting case lim

t→∞

holds.

∂ P (x, t; u) = 0 ∂t

(5.219)


159

Stability Analysis We may carry out a stability analysis of the uniform distribution as discussed in Sect. 5.1, which is based on the second variational of F . From (5.217) it is clear that the free energy KSS model is a special case of the free energy Fokker–Planck equation (5.107). Consequently, we could simply apply the results derived in Sect. 5.1.6. In what follows, however, we will reiterate the steps of the procedure outlined in Sect. 5.1.6 in order to gain more insight into the problem. To begin with, the second variation of F reads

[(x)]2 UMF (x − x )(x)(x ) dx dx . (5.220) δ 2 F [Pst ]() = Q dx + Ω Ω Ω Pst (x) Using (5.214), (5.220) gives us

2

2 ∞ 2 δ F [Pst ]() = − cn cos(nx)(x) dx + sin(nx)(x) dx Ω

n=1

Ω

2

+Q Ω

[(x)] dx . Pst (x)

(5.221)

From (5.221) we see that the set of linearly independent functions Ai (x) is given by cos(nx/2) for n = even , (5.222) An (x) = sin((n + 1)x/2) for n = odd with n = 1, 2, . . .. From (5.101) it is clear that we need to consider perturbations (x) of the form (x) =

r

a2ni [cos(ni x) − cos(ni X)st ] Pst (x)

i=1

+

r

a2ni −1 [sin(ni x)−sin(ni X)st ] Pst (x) + χ⊥ (x) Pst (x) .

i=1

(5.223) In (5.223) the indices ni correspond to nonvanishing Fourier coefficients cni . That is, we denote by Ir the set Ir = {n1 , . . . , nr } of r indices related to the d = 2r expectation values cos(ni X) and sin(ni X) that are assumed to occur in the free energy (5.217) and in the drift coefficient of the nonlinear Fokker–Planck equations (5.210). For the sake of convenience, however, we will use in what follows χ⊥ = 0 and (x) =

∞

a2n n=1 ∞

[cos(nx) − cos(nX)st ] Pst (x)

a2n−1 [sin(nx) − sin(nX)st ] Pst (x) .

+

n=1

(5.224)

160


In the case of the distribution Pst = 1/(2π) we obtain Ai = 0 and uniform Ai Ai st = δii [Ai ]2 st . Consequently, the cross-correlation matrix (5.104) assumes diagonal form and we are concerned with the special case reported in Sect. 5.1.6 that leads to (5.112-5.114). In addition, (5.224) reduces to (x) =

∞ 1 [a2n cos(nx) + a2n−1 sin(nx)] , 2π n=1

(5.225)

which corresponds to an ordinary Fourier expansion of the perturbation . In view of these considerations, it does not come as a surprise that if we substitute (5.225) into (5.221) we obtain [172] ∞ 1 δ F Pst = () = a22n cos2 (nX) st [Q − cn cos2 (nX) ] 2π n=1 2

+

∞

a22n−1 sin2 (nX) st [Q − cn sin2 (nX) ]

(5.226)

n=1

(see (5.113)), which can be transformed into ∞ 1 1 2 1 cn 2 δ F Pst = () = a2n + a22n−1 Q − 2π 2 n=1 2 2

(5.227)

because of [2π]−1 Ω cos2 (nz) dz = [2π]−1 Ω sin2 (nz) dz = 1/2. It can be seen ˜ = Q − cn /2 > 0 holds for all n, then F has a minimum from (5.227) that if λ at Pst = 1/(2π) and, consequently, the uniform probability density is asymp˜ = Q − cn∗ /2 < 0, then totically stable. If there is an index n∗ such that λ F decreases for perturbations (x) = [a2n∗ cos(n∗ x) + a2n∗ +1 sin(n∗ x)]/(2π) with a2n∗ = 0 or a2n∗ +1 = 0. This means that F has a maximum or saddlepoint at Pst = 1/(2π) and the uniform probability density is unstable. Finally, we would like to point out that using the generalized cluster amplitudes rn and cluster phases θn (5.209), the free energy (5.217) can be written as F [P ] = −

∞ 1 cn rn2 − Q BS[P ] . 2 n=1

(5.228)

Therefore, the KSS model is closely related to dynamics of cluster amplitudes. Free Energy KSS Model with Sine Coupling-force For the mean field potential UMF (x − x ) = −κ cos(x − x ) with κ ≥ 0 we find that (5.210) becomes

∂ ∂2 ∂ P (x, t; u) = κ sin(x − x )P (x , t; u) dx P + Q 2 P (5.229) ∂x ∂t ∂x Ω


and can be regarded as a free energy Fokker–Planck equation with

κ cos(x − x )P (x)P (x ) dx dx − Q BS[P ] , F [P ] = − 2 Ω Ω

161

(5.230)

F ≥ Fmin , and transient solutions that satisfy limt→∞ ∂P (x, t)/∂t = 0. From (5.213) it follows that stationary probability densities of (5.229) are described by κ Ω cos(x − x )Pst (x )dx 1 Q Pst (x) = e . (5.231) Z By means of r exp(iθ) = Ω exp(ix)P (x) dx, (5.229) can be written as ∂ ∂2 ∂ P (x, t; u) = κ r(t) sin(x − θ(t))P + Q 2 P , ∂t ∂x ∂x

(5.232)

the free energy (5.230) is found as κ F [P ] = − r2 − Q BS[P ] , 2

(5.233)

and (5.231) can be cast into the form 1 e Pst (x) = Z(rst )

κrst cos(x − θst ) Q ,

(5.234)

where Z is independent of θst : κrst cos(x) Q e dx .

Z(rst ) =

(5.235)

Ω

The stationary cluster amplitude rst corresponds to solutions m of the selfconsistency equation

exp(ix)P (x, m) dx , (5.236) m exp(iθst ) = Ω

with 1 P (x, m) = e Z

κm cos(x − θst ) Q

(5.237)

and Z given by the normalization constant Z(m) = Ω exp{κm cos(x)/Q}dx. Using the variable transformation x = x − θst , from the self-consistency equation (5.236) we obtain m = R(m) , (5.238)

162

5 Free Energy Fokker–Planck Equations with Boltzmann Statistics 1 0.8

κ>2Q

0.6 R(m) 0.4

κ 0 and R(0) = 0 hold, the self-consistency equation (5.238) is satisfied for m = 0, which tells us once more that Pst (x) = 1/(2π) describes a stationary probability density of (5.229). Solutions of (5.238) with m > 0 can be obtained by solving the self-consistency equation numerically, see Figs. 5.24 and 5.25 (bifurcation diagram). Solutions m > 0 emerge when the inequality dR(0)/dm > 1 holds. Since we have dR(0)/dm = κ cos2 (x) dx/(2πQ) = κ/(2Q), the critical parameter values


163

for κ and Q that yield dR(0)/dm = 1 are given by κ = 2Q. As far as stationary probability densities with rst = m > 0 are concerned, we realize that rst does not depend on θst . Moreover, if θst describes a stationary probability density then also θst + ∆x. The reason for this is that (5.229) is invariant under transformations x → x + ∆x. Stability Analysis Having determined the stationary distributions of the form (5.234), let us now determine their stability. From (5.227), c1 = κ, and cn>1 = 0, it follows that the stability of the uniform distribution is determined by the sign of ˜ = Q − κ/2 . λ

(5.240)

Therefore, for 2Q > κ we deal with an asymptotically stable distribution, whereas for 2Q < κ the uniform distribution is unstable. In order to examine the stability of stationary distributions with rst > 0, we use perturbations given by (x) = a1 [cos(x) − cos(X)st ] Pst (x) +a2 [sin(x) − sin(X)st ] Pst (x) + χ⊥

Pst (x) ,

(5.241)

see (5.101). Substituting (5.241) into (5.221) for cn = κ and cn>1 = 0, we obtain δ 2 F [Pst ]() = a21 Kcos,st (X)[Q − κKcos,st (X)]

+a22 Ksin,st (X)[Q − κKsin,st (X)] + [χ⊥ (x)]2 dx ,

(5.242)

Ω

where Kcos and Ksin , respectively, denote generalized variances of the form (5.46) with A(x) = cos(x) and A(x) = sin(x). Due to the aforementioned invariance of (5.232) under transformations x → x+∆x, all distribution (5.234) with a particular rst but different θst have the same stability properties. For this reason, in what follows we study the case θst = 0, that is, distributions that are given by Pst = Z −1 exp{κrst cos(x)/Q} and satisfy Pst (x) = Pst (−x). In this case, (5.241) and (5.242) read (x) = a1 [cos(x) − rst ] Pst (x) + a2 sin(x)Pst (x) + χ⊥ Pst (x) (5.243) and δ 2 F [Pst ]() = a21 Kcos,st (X)[Q − κKcos,st (X)]

+a22 sin2 (X) st [Q − κ sin2 (X) st ] + [χ⊥ (x)]2 dx Ω

and we obtain the stability coefficients

(5.244)

164


˜ 1 = Q − κKcos,st (X) , λ ˜ 2 = Q − κ sin2 (X) . λ st

(5.245) (5.246)

˜ 1 and λ ˜ 2 reduce to (5.240) for Pst = 1/(2π). Let us evaluate the Note that λ ˜ expression λ2 = Q − κ sin2 (X) st for Pst = Z −1 exp{κrst cos(x)/Q}. First, the second derivative of the exponential function exp{κrst cos(x)/Q} reads d2 κrst cos(x)/Q κrst cos(x) κrst cos(x)/Q e =− e Q dx2 2 κrst sin2 (x)eκrst cos(x)/Q . + Q

(5.247)

Integrating this equation with respect to x and dividing it by Z yields Q = κ sin2 (X) st . (5.248) Consequently, for Pst (x) = Z −1 exp{κrst cos(x)/Q} we have ˜2 = 0 λ

(5.249)

and the second variation of F reads

δ 2 F [Pst ](a1 , a2 , χ⊥ ) = a21 Kcos,st (X)[Q − κKcos,st (X)] +

[χ⊥ (x)]2 dx . Ω

(5.250) Using the stability coefficient (5.245), we draw the following conclusions. For ˜ 1 > 0 the free energy F increases for all small perturbations = 0 with λ a2 = 0 because if a2 = 0 we have a1 = 0 or χ⊥ = 0. Perturbations with a1 = 0, χ⊥ = 0, and a2 = 0 given by (x; a2 ) = a2 sin(x)Pst (x)

(5.251)

yield δ 2 F = 0 and do not lead to a change F up to the order 2 . Let us illustrate this issue from another perspective. First, we note that a shifted distribution Pst (x + ∆x) can be written as a Taylor expansion like Pst (x − ∆x) = exp{−∆x d/dx}Pst (x). For Pst (x) = Z −1 exp{κrst cos(x)/Q} we get Pst (x−∆x) = Pst (x)+κrst ∆xQ−1 sin(x)Pst (x)+w(x, ∆x), where w ∝ O(∆x2 ). Let us put a2 = κrst ∆xQ−1 . Then, we have Pst (x − Qa2 /[κrst ]) = Pst (x) + a2 sin(x)Pst (x) + w(x, Qa2 /[κrst ]), where w ∝ O(a22 ). Since a2 is assumed to be a small parameter, we are allowed to add on the right-hand side of (5.251) an expression of order a22 and of higher order without changing the results previously derived by means of linear stability analysis. That is, we add now the function w(x, Qa2 /[κrst ]) on the right-hand side of (5.251) and consider the perturbation (x; a2 ) = a2 sin(x)Pst (x) + w(x, Qa2 /[κrst ]): Pst (x) + (x; a2 ) = Pst (x − Qa2 /[κrst ]) =

1 eκrst cos(x − a2 )/Q , Z(rst ) (5.252)


165

with a2 = a2 Q/(κrst ) and Pst (x) = Z −1 exp{κrst cos(x)/Q}. That is, the perturbation simply yields a translation of the distribution Pst (x) and a shift of the cluster phase θst from θst = 0 to θst = a2 , whereas the cluster amplitude rst is not affected by the perturbation. In sum, we conclude that the perturbation (5.251) does not change F up to the order 2 because F is invariant under translations x → x + ∆x and the perturbation (5.251) basically induces such a translation. As a result, ˜ 1 > 0 but not the stationary distribution (5.234) with θst = 0 is stable for λ asymptotically stable. We would like to point out that this result carries over to the case of stationary distributions (5.234) with θst = 0 (as explained above). In other words, we may regard the distributions (5.234) as a oneparametric family of distributions with a continuous parameter θst ∈ [0, 2π). ˜ 1 > 0 this one-parametric family of distributions describes a “valley” of For λ the free energy measure (5.233) and therefore every member of this family corresponds to a stable but not asymptotically stable stationary distribution (see (5.13) and Sect. 5.1). ˜ 1 > 0 all perturbations of the distributions Pst (x) given by (5.234) For λ decrease as a function of time expect those related to a change of the cluster ˜ 1 < 0 perturbations with a1 = 0 increase as a phase θst . In contrast, for λ function of time and the stationary distributions Pst (x) are unstable. Using dR κ = Kcos,st (X) , dm Q ˜ 1 as we can write λ

(5.253)

dR ˜1 = Q 1 − λ , dm m=rst

(5.254)

which implies that stationary probability densities with dR/dm > 1 at m = rst correspond to unstable distribution, whereas distributions with dR/dm < 1 at m = rst correspond to stable ones. Then, from Fig. 5.24 we read off that if the self-consistency equation exhibits multiple solutions we have dR/dm > 1 at m = 0 and dR/dm < 1 at m > 0. Since (5.245) and (5.254) reduce to (5.240) for Pst = 1/(2π), the nonlinear Fokker–Planck equation (5.229) exhibits for κ < 2Q an asymptotically stable uniform stationary distribution. For κ > 2Q the KSS model (5.229) exhibits an unstable uniform stationary distribution and a family of stable (but not asymptotically stable) nonuniform stationary distribution functions given by (5.234) with rst > 0 and arbitrary θst . These findings are summarized in the bifurcation diagram depicted in Fig. 5.25. In closing our considerations about the KSS model, let us illustrate that for the sine coupling-force the bifurcation from a uniform to a nonuniform stationary distribution indeed results from the fact that a free energy minimum becomes a free energy saddle point or maximum. To this end, we consider the one-parametric family of probability densities

166


κ2Q

–1.86 –1.88 0

0.2

0.4

0.6

0.8

c

1

Fig. 5.26. Free energy (5.256) as a function of the parameter c. For Q = 1 two cases are shown: κ = 1 and κ = 2.5. For κ = 2.5 there is a minimum at cmin ≈ 0.6 (which corresponds to the intersection point at m ≈ 0.6 in Fig. 5.24) [171]

Pc (x; θ) = with c ∈ [0, 1] and Z = into (5.233), we obtain

Ω

1 exp Z

κc cos (x − θ) , Q

(5.255)

exp{κc cos(x)/Q} dx [171]. Substituting (5.255)

22 κ1 cos(X)Pc (x;0) + κc cos(X)Pc (x,0) 2

κc cos(x) dx , exp −Q ln Q Ω

F (c) = −

(5.256)

where averages are computed from (5.255) with θ = 0. Differentiating (5.256) with respect to c, gives us 1 2 d κ2 F (c) = Kcos (X)Pc (x;0) c − cos(X)Pc (x;0) . dc Q

(5.257)

For c = 0 we have dF/dc = 0 because of c − cos(X) = 0 for c = 0, which means that the free energy F (c) is stationary at the uniform distribution. In order the check whether this critical point corresponds to a maximum or a minimum, we differentiate F with respect to c again. Thus, we obtain d2 κ κ2 K 1 − F (c) = (X) (X) K cos cos Pc (x;0) Pc (x;0) dc2 Q Q 9 : d + c − cos(X)Pc (x;0) Kcos (X)Pc (x;0) . (5.258) dc For the uniform distribution (i.e. for c = 0) we obtain Kcos = 1/2 and (5.258) reads d2 κ κ2 1 − . (5.259) F (c) = dc2 2Q 2Q c=0


167

It is clear from (5.259) that for κ < 2Q the free energy F (c) has a minimum at c = 0. This is a necessary condition for F [P ] to exhibit a minimum at Pst = 1/(2π) with respect to the whole function space of probability densities. Furthermore, as shown in Fig. 5.26, for κ < 2Q the function F (c) increases monotonically. That is, there is no further minimum. For κ > 2Q the function F (c) has a maximum at c = 0, which implies that F [P ] has a maximum or a saddle point at P = 1/(2π) with respect to the whole function space of probability densities. As shown in Fig. 5.26, for κ > 2Q a new minimum emerges at c = cmin . This minimum describes a family of stable stationary probability density given by (5.234) with rst = cmin and arbitrary θst . 5.3.3 Mean Field Haken–Kelso–Bunz (HKB) Model – Cluster Phase Dynamics As mentioned earlier, the KSS model with a sine coupling-force (5.229) is invariant under transformations x → x + ∆x. In this section we break this invariance. To this end, we supplement (5.229) with a drift force h(x) that is not invariant under the transformation x → x + ∆x. We consider a force h(x) that has attractive points x∗i ∈ Ω (i.e., we have h(x∗i ) = 0 and dh(x∗i )/dx < 0). In doing so, we assume that the deterministic evolution equation dq(t)/dq = h(q) of a dynamical system has stable fixed points at q = x∗i . In this case, h(x) “pins” the state variable q(t) of the system to a fixed point x∗i and is referred to as a pinning force. As a pinning force we choose h(x) = −α sin(x) − 2β sin(2x), which gives us the nonlinear Fokker–Planck equation ∂ P (x, t; u) ∂t

∂2 ∂ α sin(x) + 2β sin(2x) + κ = sin(x − x )P (x , t; u) dx P + Q 2 P , ∂x ∂x Ω (5.260) with κ ≥ 0 and α, β ≥ 0 [198, 199]. The pinning force h(x) can be regarded as the force h(x) = −dVHKB /dx of the potential VHKB (x) = −α cos(x) − β cos(2x) .

(5.261)

The potential VHKB was introduced by Haken, Kelso, and Bunz [259, 264, 335] in biophysics, which is the reason why we will refer to (5.260) as mean field HKB model. We would like to point out that the model given by (5.260) can also be regarded as a generalization of the stochastic HKB model proposed by Sch¨ oner et al. [512], which has been extensively studied in the literature, see, for example, [16, 111, 214, 461, 487]. The potential VHKB has extrema at x = 0 and x = ±π. For α < 4β there are two additional extrema at cos(x) = −α/(4β). For α < 4β the potential is bistable, exhibits minima

168


at x = 0 and x = ±π and has two maxima related to cos(x) − α/(4β), see Fig. 5.27. For α ↑ 4β the maxima merge with the minima at ±π. For α > 4β the potential is monostable and exhibits a minimum at x = 0 and two maxima at x = ±π, see Fig. 5.27.

V(x)

V(x)

x

α/(4β)1

Fig. 5.27. HKB potential for several ratios α/(4β) and x ∈ [−π, π]

We anticipate that the mean field HKB model exhibits two qualitatively different parameter regimes. First, there should be a parameter regime with two stable distributions related to the minima at x = 0 and x = π (or x = −π) of the potential VHKB for α < 4β. Second, there should be a parameter regime with a single stable distribution related to the unique potential minimum of VHKB at x = 0 for α > 4β. Consequently, we anticipate that the model describes a phase transition between a bistable and a monostable regime. This behavior should arise from the interplay between the potential VHKB and the mean field coupling term hMF (x) = −κ sin(x − x ). The idea is that the HKB potential makes the system potentially bistable, whereas the mean field coupling term transforms this potential bistability into an actual bistability by forcing the subsystems k (represented by the realizations X k ) of a many-body system to assume a common phase. Equation (5.260) is the free energy Fokker–Planck equation (5.3) for

κ F [P ] = VHKB (x)P (x) dx − cos(x − x )P (x)P (x ) dx dx − Q BS[P ] . 2 Ω Ω (5.262) The free energy is of type E in Table 4.2, which implies that the inequality F ≥ Fmin and the limiting case limt→∞ ∂P (x, t; u)/∂t= 0 holds (H-theorem, see Sect. 4.3). From (5.8) and δU/δP = VHKB (x) − κ Ω cos(x − x )P (x ) dx it follows that VHKB (x) − κ Ω cos(x − x )Pst (x ) dx − 1 Q Pst (x) = e . (5.263) Z Furthermore, (5.260) can be written as a special case of (5.107):


169

∂ P (x, t; u) = ∂t ∂ [α sin(x) + 2β sin(2x) + κ (sin(x) cos(X) − cos(x) sin(X))] P ∂x ∂2 +Q 2 P (5.264) ∂x with

F [P ] =

VHKB (x)P (x) dx− Ω

2 κ1 2 2 cos(X) + sin(X) −Q BS[P ] . (5.265) 2

Then, stationary solutions can be obtained from (5.109) and satisfy 1 − Pst (x) = e Z

VHKB (x) − κ (cos(x) cos(X)st + sin(x) sin(X)st ) Q . (5.266)

In order to determine cos(X)st and sin(X)st , we define VHKB (x) − κ (cos(x)m1 + sin(x)m2 ) − 1 Q P (x, m) = , e Z(m)

− VHKB (x) − κ (cos(x)m1 + sin(x)m2 ) Q e Z(m) = dx , (5.267) Ω

for m = (m1 , m2 ) and use R = (R1 , R2 ) given by

R1 (m) = cos(x)P (x, m) dx , R2 (m) = sin(x)P (x, m) dx Ω

(5.268)

Ω

to write the self-consistency equation m = R(m) .

(5.269)

Then, solutions of (5.269) yield cos(X)st = m1 and sin(X)st = m2 . Stability Analysis It is clear from (5.265) that the second variation of F does not depend on the linear term Ω VHKB (x)P (x) dx and therefore is equivalent to δ 2 F of the free energy equation (5.230) of the KSS model with sine coupling-force. Using (5.221) for c1 = κ and cn>1 = 0, the second variation reads explicitly

2

δ 2 F [Pst ]() = −κ

cos(y)(x) dy

+Q Ω

Ω

2

+

sin(y)(x) dy Ω

2

[(x)] dy . Pst (x)

(5.270)

Substituting perturbations given by (5.241) into (5.270), we obtain (5.242).

170


Symmetric Stationary Solutions From the symmetry of the potential VHKB (x) given by V (HKB (x) = VHKB (−x) it follows that R2 (m1 , 0) = 0 and, consequently, we can study solutions of (5.269) of the form (5.271) m2 = 0 , m1 = R1 (m1 , 0) . In this case, we are dealing with symmetric stationary solutions that satisfy 1 − Pst (x) = = e Z

VHKB (x) − κ cos(x) cos(X)st Q .

(5.272)

That is, the symmetry of the potential VHKB determines the symmetry of a class of stationary probability densities of the mean field HKB model (5.260). Note that if we are dealing with a pinning force h(x) that satisfies h(x∗ + ∆x) = −h(x∗ − ∆x) and is related to a symmetric potential around x∗ = 0, then the mean field HKB model would exhibit stationary probability densities satisfying Pst (x∗ + ∆x) = Pst (x∗ − ∆x). In order to determine the stability of the distributions (5.272), we proceed as in the case of the KSS model with sine coupling-force. For symmetric solutions (5.272) the perturbation (5.241) reads (x) = a1 [cos(x) − rst ] Pst (x) + a2 sin(x)Pst (x) + χ⊥ Pst (x) , (5.273) with rst = Ω cos(x)Pst (x) dx. Likewise, (5.242) becomes δ 2 F [Pst ]() = a21 Kcos,st (X)[Q − κKcos,st (X)]

2 2 2 +a2 sin (X) st [Q − κ sin (X) st ] + [χ⊥ (x)]2 dx .

(5.274)

Ω

Using ˜ 1 = Q − κKcos,st (X) , λ ˜ 2 = Q − κ sin2 (X) , λ st

(5.275) (5.276)

the stability of symmetric stationary probability densities can be conveniently ˜ 1 > 0 and λ ˜ 2 > 0, then stationary solutions (5.272) are determined. If λ ˜ 1 < 0 or λ ˜ 2 < 0, then distributions of the form asymptotically stable. If λ (5.272) are unstable. ˜ 1 and λ ˜ 2 ? In What is the nature of the stability conditions related to λ ˜ 1 and λ ˜ 2 to bifurcations of the cluster amplitude what follows, we will relate λ and the cluster phase of symmetric stationary probability densities (5.272) in particular and of stationary probability densities of the mean field HKB model (5.260) in general.


171

Cluster Amplitude and Cluster Phase Description Using (5.204), we transform (5.260), (5.265), and (5.266) into ∂ ∂ ∂2 P (x, t; u) = [α sin(x) + 2β sin(2x) + κr(t) sin(x − θ(t))] P + Q 2 P , ∂x ∂t ∂x (5.277)

κ 2 F [P ] = VHKB (x)P (x) dx − r [P ] − Q BS[P ] , (5.278) 2 Ω and

VHKB (x) − κrst cos(x − θst ) 1 − Q Pst (x) = e . Z It is helpful to rescale these equations by means of α β κ ˜ = , β˜ = , P˜ (x, t˜; u) = P (x, t; u) . t˜ = Qt, κ ˜= , α Q Q Q

(5.279)

(5.280)

Moreover, let us introduce the force ˜ h(x) = −˜ α sin(x) − 2β˜ sin(2x)

(5.281)

VHKB (x) = −˜ α cos(x) − β˜ cos(2x) V˜HKB (x) = Q

(5.282)

and the potential

of the deterministic HKB model d ˜ ˜ q(t) = h(q) dt˜

(5.283)

with respect to the rescaled variables. Then, we have 2 ∂ ˜ ˜ ∂2 ˜ ∂ 1 α ˜ sin(x) + 2β˜ sin(2x) + κ ˜ r(t˜) sin(x − θ(t˜)) P˜ + P (x, t; u) = P ∂x ∂x2 ∂ t˜ (5.284) for r(t˜) exp{iθ(t˜)} = Ω exp{ix}P˜ (x, t˜, u) dx and 1 ˜ ˜ rst cos(x − θst ) . P˜st (x) = e−VHKB (x) + κ Z

(5.285)

Saddle Node Bifurcation of rst

For the sake of convenience, we introduce now a modified cluster phase θ ∈ [0, by r (t˜) exp{iθ (t˜)} = π) and a signed cluster amplitude r ∈ [−1, 1] defined exp{ix}P˜ (x, t˜; u) dx. Note that the variables θ and r , on the one hand, Ω

172


and the variables θ and r, on the other hand, are only different with respect to their domains of definition. For the stationary case this implies: rst ≥ 0 , θst =0, θst = 0 ⇒ rst = rst ≥ 0 , θst = π ⇒ rst = −rst ≤ 0 , > 0 ⇒ θst = 0 , rst < 0 ⇒ θst = π . rst

(5.286)

In addition, (5.285) reads 1 ˜ P˜st (x) = e−VHKB (x) + κrst cos(x − θst ) , Z

(5.287)

with θst ∈ [0, π). In order to examine symmetric stationary solutions of the form (5.272), we impose a symmetry constraint on (transient and stationary) solutions of (5.284): P˜ (x, t˜; u) = P˜ (−x, t˜; u) . (5.288) ˜ In this case, from r(t˜) exp{iθ(t˜)} = Ω exp{ix}P (x, t˜, u) dx it follows that θ can assume only two values, namely, θ(t˜) = 0 and θ(t˜) = π, and that θ and, in particular, θst are fixed by θ = θst = 0. The objective is to determine stationary solutions of (5.284) and their stability under the constraint (5.288). From (5.287) and θst = 0 we can derive the self-consistency equation

˜ , m = R(m; κ ˜, α ˜ , β)

(5.289)

for m ∈ [−1, 1] with

˜ = R(m; κ ˜, α ˜ , β)

cos(x)P˜ (x, m) dx , Ω

P˜ (x, m) =

1 ˜ e−VHKB (x) − κm cos(x) . Z(m)

(5.290)

Then, the cluster amplitude rst occurring in (5.287) corresponds to solutions of (5.289). One can verify that R satisfies the following properties:

– R(x; . . .) is a monotonously increasing but bounded function in x ∈ [−1, 1]: |R(x; ·)| ≤ 1

and

d R(m; ·) = κ ˜ Kcos ≥ 0 , dm

(5.291)

with Kcos defined by (5.46). In particular, for P˜ (x, m) = δ(x) and P˜ (x, m) = δ(x ± π) we have |R| = 1, whereas for P˜ (x, ·) ∈ C 0 (Ω) we have |R| < 1.


–

–

173

We have

∂ ˜ = m˜ R(m; κ ˜, α ˜ , β) κKcos . ∂˜ κ R is a monotonically increasing function with respect to α: ˜ ∂ ˜ = Kcos ≥ 0 . R(m; κ ˜, α ˜ , β) ∂α ˜

(5.292)

(5.293)

Having discussed some general properties of R, let us consider now the solu tion m = rst = 0 of the self-consistency equation (5.289). Since for α ˜ = 0 we have

(5.294) cos(x) V˜HKB (x) dx = 0 , Ω

from (5.290) and (5.282) we conclude that ˜ =0. R(m; κ ˜, α ˜ = 0, β)

(5.295)

Consequently, rst = 0 solves the self-consistency equation (5.289) for α ˜ = 0 and the corresponding stationary probability density can be calculated from (5.287). From (5.291), (5.293) and (5.295) we further conclude that for α ˜ > 0 there exists at least one positive solution of (5.289). In order to see this recall that, as shown above, for α ˜ = 0 we have R(m = 0; ·) = 0. For increasing α ˜ , (5.293) results in R(m = 0; ., a ˜ > 0, .) > 0. Since R is a monotonously increasing function with |R| < 1, there must be at least one intersection point between the graph of m → R(m; ., α ˜ > 0, .) and the diagonal of the (m, R)-plane within the range m ∈ [0, 1] that corresponds to a positive solution rst . According to (5.286), this implies the existence of ˜ smaller than a a stationary probability density (5.285) with θst = 0. For α critical value α ˜ c we obtain two negative solutions of (5.289), which merge for ˜ ˜>α ˜ c . Figure 5.28c shows R(m; κ ˜, α ˜ , β) α ˜=α ˜ c and entirely disappear for α ˜ α assume fixed values. The for three values of α ˜ while κ ˜ and the ratio 4β/˜ intersection points of the solid lines and the diagonal represent the solutions of (5.289). The figure illustrates that for α ˜ > 0 an intersection point with m > 0 always exists. Now that the existence of stationary probability densities has been demonstrated, we need to determine their stability. Analogously to (5.252), we can show that the perturbation (5.273) of a stationary probability density (5.290) for a2 = 0, a1 = 0, and χ⊥ = 0 results in a shift of the cluster phase θst from θst = 0 to θst = 0. Since we have frozen the cluster phase θst by the constraint (5.288) such perturbations are forbidden and the stability is exclusively determined by the coefficient λ1 given in (5.275). From (5.275), (5.280), and (5.291) it follows that dR ˜ λ1 = Q 1 − . (5.296) dm m=rst

174


(a)

(b) ∼ α

8 6 ∼ α

2.5

4

2.0

2

1.5

0 10 8 6 ∼ κ 4 2

1.0

monostable region

0.5

0

0.5 1

1.5 2

bistable region 0.5

2.5 3

1.0

1.5

2.0

2.5

e

(c)

e

(d) initial

R 0.5

P

III 0.0

II

1.0 0.5

-0.5

I

0 -1

-0.50

0.00

0.50

m

-0.5

0

x/ π

0.5

1.0 1.05 1.10 ∼ 1.15 α 1.20 1

Fig. 5.28. Panel (a): three-dimensional plot of the critical parameter α ˜ versus κ ˜ and e = 4α/ ˜ β˜ with α ˜ > 0 as calculated from (5.298). The surface represents the bifurcation points of a saddle node bifurcation in the parameter space (˜ κ, α, ˜ e) and divides the parameter space into a monostable and a bistable region. Panel (b): a cut through the surface of Fig. 5.28a at κ ˜ = 4. Panel (c): illustration of the selfconsistency equation (5.289). Solid lines: R(m) defined by (5.290) for three different values of α ˜ (0.5, 1.1 and 2.0) and κ ˜ = 4, e = 1. Dashed line: diagonal of the (R, m) plane. Panel (d): simulation of the mean field model (5.284) under the constraint c 2000, with permission from Elsevier (5.288); reprinted from [198],

Consequently, from Fig. 5.28c we read off that the stationary probability density that corresponds to the intersection point with m = rst > 0 represents an asymptotically stable solution. Likewise, the two negative solutions of (5.289) represent an asymptotically stable and an unstable solution. The vanishing of this pair of solutions reveals a saddle node bifurcation. Having obtained the self-consistency equation (5.289), we can numerically compute the number of positive and negative solutions for every particular ˜ For the sake of convenience, we introduce the parameter e = triple (˜ κ, α ˜ , β).


175

˜ α ≥ 0 (which implies β˜ = α 4β/˜ ˜ e/4 for α ˜ ≥ 0, e ≥ 0) and use the HKB potential (5.282) described by 9 : e V˜HKB (x) = −˜ α cos(x) + cos(2x) . (5.297) 4 In the parameter space spanned by the parameters κ ˜, α ˜ , e a surface can be identified that divides the parameter space into two regions: a region which < 0) and a positive solution (rst > allows for two negative solutions (rst 0) and another region which only allows for a single positive solution. The surface in Fig. 5.28a represents those points (˜ κ, a ˜, e) at which both negative solutions of (5.289) merge into a single solution. As a result, the points on the surface satisfy the relations: rst ; ·), = R(rst

d R(m; ·)|m=r = 1, st dm

rst 0 holds for determined by the sign of λ distributions (5.290) with rst > −˜ α/κ. By analogy to (5.248), one finds for rst > −˜ α/˜ κ, α ˜ > 0, and β˜ = 0 that

sin2 (X) st =

rst 1 . < κ α ˜+κ ˜ rst ˜

(5.299)

If β˜ is increased then the distributions (5.290) become smaller at positions x for which sin2 (x) is large (e.g., at x = π/2 and x = 3π/2) and become larger at positions sin2 (x) is small (e.g., atx = 0 and x = ±π). 2for which Consequently, sin (X) st for β˜ > 0 is smaller than sin2 (X) st for β˜ = 0 and we conclude that 2 1 sin (X) st < , (5.300) κ ˜ for all symmetric stationary distributions with β˜ ≥ 0, α ˜ > 0, and rst > −˜ α/˜ κ. ˜ Finally, for β → ∞ all distributions satisfying (5.290) reduce to a delta distribution with peaks at x = 0 and x = ±π. Therefore, sin2 (X) st = 0 for β˜ → ∞. ˜ 2 > 0 for r > −˜ α/˜ κ. From (5.276), (5.280), and (5.300), it is clear that λ st Consequently, the symmetric distribution (5.285) with θst = 0 (i.e., the distri bution (5.287) with θst = 0 and rst > 0) is asymptotically stable. In contrast, distributions (5.285) with θst = π (i.e., distributions (5.287) with θst = 0 ˜2. ˜ 1 > 0 can yield both positive and negative values for λ and rst < 0) and λ Therefore, they may correspond to asymptotically stable or unstable distributions if we dispense with the symmetry condition (5.288). We will examine this issue next. Stationary Solutions (5.285) with θst = ±π We study now the stability of stationary solutions of the form (5.285) with θst = π (or likewise θst = −π). We will illustrate that in a particular range of the parameter space, stationary probability densities with θst = π that have been considered in the preceding as asymptotically stable solutions become unstable if we omit the symmetry constraint (5.288) and take perturbations of the cluster phase θ into account. This change of stability will be interpreted in terms of a pitchfork bifurcation and investigated in two distinct ways: linear stability analysis and the branching of stationary solutions in the function space of probability densities. Linear Stability Analysis Since perturbations of asymptotically stable distributions vanish, deviations from such distributions vanish in the long time limit. In particular, expectation values describing theses deviations vanish for t → ∞. Therefore, a


177

necessary condition for a stationary distribution to correspond to an asymptotically stable one is that expectation values of perturbations vanish for t → ∞. In contrast, if there is at least one expectation value that describes a perturbation and increases with time, we have a strong indication that the norm of the perturbation increases and the distribution is an unstable one, see (5.16). In order to examine the stability of distributions (5.285) with θst = π, we introduce the mean deviation ∆x (t˜) given by

2π (5.301) (x − π)P˜ (x, t˜) dx = M1 (t˜) − π , ∆x (t˜) = 0

which can be regarded as a shifted first moment M1 (t˜) as indicated. At the instance t0 we consider a perturbation of the probability density P˜st (x; θst = π) defined by (5.285), which yields u(x) = P˜st (x − (t˜0 ); θst = π) ,

(5.302)

where (t0 ) is a small number. We can verify that (5.302) exhibits the cluster phase θ = π + (t˜0 ) . (5.303) From (5.301) and (5.302) we can determine ∆x at time t˜0 and obtain by means of partial integration 1 2 ∆x (t˜0 ) = 1 − 2π P˜st (0; θst = π) + O(2 ) . (5.304) Using (5.285), (5.301), and (5.302), we can determine the evolution of ∆x (t˜) at t˜ = t˜0 :

2π ˜ d dh(x) ˜ ∆x (t˜) = (5.305) Pst (x; ·) dx + O(2 ) , dx dt˜ 0 t˜=t˜0 ˜ given by (5.281). Neglecting higher order terms of and combining with h (5.304) and (5.305) results in d ∆x (t˜) = λθst=π ∆x (t˜0 ) , (5.306) dt˜ t˜=t˜ 0

where λθst=π is defined by

˜ dh(x) dx P˜st (x; θst = π) 1 dx Ω λθst=π = = . 1−2π P˜st (0; θst = π) 1−2π P˜st (0; θst = π) (5.307) Equation (5.306) can be further evaluated for the important special case of unimodal distributions (5.285) that decrease monotonously on either side of the maximum located at x = π and satisfy B

˜ dh(x) dx

C

178


d ˜ Pst (x) = dx

0 for x = 0 ∨ x = π . c > 0 for x ∈ (0, π)

(5.308)

Note that the symmetry of the HKB potential implies that dP˜st (x)/dx = −dP˜st (x − π)/dx < 0 holds for x ∈ (π, 2π). The condition (5.308) is satisfied only for αeff = α ˜ − rst κ ˜ < 0 and |αeff | > 4β˜ (because in this case the corresponding effective potential Veff (x) = V˜HKB (x) − κ ˜ rst cos(x) occurring in (5.287) has a unique minimum at x = π). Since (5.308) holds, the shifted initial probability density u(x) exhibits a unique maximum. The evolution of the mean deviation ∆x at the instance t˜0 may indicate whether or not the position of the maximum of u(x) relaxes back towards π at time t˜0 . From (5.308) and the normalization of P˜ (x, θst = π) it follows that the inequality P˜ (0, ·) < 1/2π holds. Consequently, the denominator in (5.307) is positive. With (5.307) at hand, we realize that a stationary probability density that is regarded as an asymptotically stable solution under the constraint (5.288) can also become unstable. For a Lyapunov exponent λθst =π > 0 we deal with an unstable stationary solution, whereas λθst =π < 0 means that P˜st (x, θst = π) satisfies a necessary condition for an asymptotically stable stationary solution. We would like to point out that in the limit of vanishing noise, all unimodal stationary probability densities of the from P˜st (x, θst = π) reduce to a delta distribution with a peak at x = π (i.e., we have P˜st (x; θst = π) = δ(x − π) and P˜st (0; θst = π) = 0). Then, the averaging in (5.307) can be replaced by the evaluation of the expression within the brackets at x = π and we obtain ˜ λθst =π = dh(π)/dx, which means that we obtain the Lyapunov exponent of the deterministic HKB model (5.283) with respect to the stationary point qst = π. Branching of Stationary Solutions We now draw attention to the special case in which a change of stability is mediated by a pitchfork bifurcation. We first note that in view of the symmetry and periodicity of the HKB potential (5.282) we conclude that if the pair (rst , θst = π + ∆) describes a stationary probability density (5.285), then (5.285) for (rst , θst = π − ∆) describes a stationary distribution as well. Let us rewrite the self-consistency equation rst exp{iθst } = Ω exp{ix}P˜st (x) dx in terms of the functions f and f :

˜ κ f (rst , θst , α ˜ , β, ˜) = sin(x−θst )P˜st (x) dx = 0 , (5.309)

˜ κ ˜ , β, ˜ ) = rst − cos(x−θst )P˜st (x) dx = 0 . (5.310) f (rst , θst ; α For critical parameters α ˜ c , β˜c , and κ ˜ c that describe a pitchfork bifurcation point, we consider the normal form f (rst , θst ; α ˜ c , β˜c , κ ˜ c ) ∝ (θst − π)3 that yields


∂ ˜c ) = 0 . f (rst , θst ; α ˜ c , β˜c , κ ∂θst

179

(5.311)

From (5.285), (5.309), and (5.311) we obtain 1−

2 = cos(2X)st,c , κ ˜c

(5.312)

which can equivalently be expressed as

1 sin2 (X) st,c = , κ ˜c

(5.313)

where averaging is carried out with respect to the stationary probability density (5.285) at the bifurcation point described by α ˜ c , β˜c , κ ˜ c , and θst = π. Note that we have derived this result for all kinds of symmetric distributions (5.285) with θst = π that do not necessarily satisfy (5.308). From (5.280) and (5.313) it follows that a pitchfork bifurcation point of a symmetric stationary distribution with θst = π is described by the condition ˜ 2 vanishes, see (5.276). On account κ sin2 (x) st = Q. For this condition λ of the result obtained from the linear stability analysis of ∆x, the analysis of (5.309), and the observation mentioned earlier that perturbations related ˜ 2 shift the cluster phase θst of stationary distributions, we have strong to λ ˜ 2 corresponds to support for the hypothesis that the stability coefficients λ the control parameter of a pitchfork bifurcation. In order to demonstrate that we are indeed dealing with a pitchfork bifurcation, we solved numerically (5.309) and (5.310) for a particular value of κ ˜ (˜ κ = 4) and thus obtained the cluster phases θst and cluster amplitudes rst . Figure 5.29c) depicts the solutions θst of (5.309) and (5.310). Note that Fig. 5.29c) does not show the solutions that corresponds to the unstable station ary probability density with dR(m)/dm and m = rst < 1. There are two side branches with θst = π ± ∆ that merge at ec with the solution θst = π. The critical value ec of about ec ≈ 1.6 (panel b) coincides with the critical value derived by the linear stability analysis (see below). Branching of Solutions and Convolution Integrals Emergence and vanishing of the side branches become transparent for the HKB potential (5.282) when interpreting (5.309) as the convolution of an odd function g(x) and an even function u(x). Substituting (5.282), (5.285), and z = x − θst into (5.309) we obtain:

0=f = g(z)u(z−θst ) dz , (5.314) Ω

with ˜ cos(x) + β˜ cos(2x) . ˜ rst cos(x) , u(x) = eα g(x) = sin(x) eκ

(5.315)

180


(a)

(b)

8

∼ α

6 ∼ α

2.5

4

2.0

2

1.5

0 10 8 6 ∼ κ 4 2

monostable region

1.0

bistable

0.5

region 0

0.5 1

1.5 2

2.5 3

0.5

1.0

1.5

2.0

2.5

e

(c)

e

(d)

x / 2π

initial

0.75

P

0.50 (unstable)

(stable)

1.0 0.5

0.25

0

(stable)

-1

1.50

2.00

2.50

e

-0.5

0

x/ π

0.5

1.8 1.7 1.6 1.5 e 1.4 1

Fig. 5.29. Panel (a): the “roof-like” surface describes a saddle node bifurcation just as in Fig. 5.28a); “wall-like” surface represents the critical points of pitchfork bifurcations. Panel (b): the cut through the surface of Fig. 5.29a) at κ ˜ = 4. Panel (c): stationary cluster phases θst calculated from (5.309) and (5.310) for several e with κ ˜ = 4, α ˜ = 0.5. Panel (d): simulation of the mean field HKB model (5.284); c 2000, with permission from Elsevier reprinted from [198],

Due to the symmetry properties of g(x) and u(x), the integral relation (5.314) is solved in any case by θst = 0 and θst = π. It is clear from Fig. 5.27 that for 4β˜ ≤ α ˜ the function u(x) exhibits a unique maximum at the origin and decreases monotonously on both sides of that maximum. Since g(z) is a antisymmetric function, the convolution integral vanish only if u(z − θst ) is a ˜ α ≤ 1 the integral (5.314) only admits symmetric function. That is, for 4β/˜ the solutions θst = 0 and θst = π. In order to study the parameter range ˜ α ∈ (1, ∞), we first consider the case α 4β/˜ ˜ = 0. In this case the function u(z) reduces to u (z) = exp[β˜ cos(2z)] and, consequently, (5.314) is also solved by θst = ±π/2. Figure 5.30 shows g(z) and z → u (z − π/2) for some typical


181

parameter values1 . If we increase α ˜ , the degeneration of the two maxima at ±π/2 of z → u(z − π/2) disappears. To satisfy (5.314), the larger maximum of the non-degenerated function has to be shifted into the shallower region of g(z) by shifting the whole function. Hence, θst differs from ±π/2. Without any loss of generality, let us assume that the maximum at π/2 is higher than the maximum at −π/2 (which is the case shown in Fig. 5.30). In that case, we have to shift the absolute maximum from π/2 towards π, and, consequently, the whole function shifts towards the right-hand side. Figure 5.30 shows an example of a function u(z − θst ), where θst > π/2 has been chosen such that the integral over the product g(z)u(z − θst ) vanishes (the integral relation ˜ α ∈ (1, ∞) (5.314) is satisfied). Therefore, we conclude that in the range 4β/˜ the additional solutions θst = π ± ∆ (given that they exist) are restricted by ˜ α ∈ (1, ∞) the deviation ∆ characterizing the ∆ ∈ [0, π/2]. In sum, for 4β/˜ ˜ α decreases side branches decreases from ∆ = π/2 to ∆ = 0 when e = 4β/˜ from ∞ to ec ≥ 1. The additional solutions with ∆ = 0 are considered as the unstable side branches of a pitchfork bifurcation (see Fig. 5.29c).

6

g

4 2 –1 –0.8

–0.4

0 –2

u’ 0.4

u

0.8 1 x /π

Fig. 5.30. Interpretation of (5.309) as equating a convolution integral to zero. The solid line labeled g represents g(z) with κ ˜ = 4 and rst = 0.77. The lines labeled u and u represents z → u = u(z − θst ) for β˜ = 0.375, α ˜ = 0, and θst = π/2 and z → u(z − θst ) for β˜ = 0.375, α ˜ = 0.5, and θst = 2.26. The integrals over the products g u and g u vanish. The shifts of the maxima of u and u with respect to the origin represent possible stationary cluster phases that satisfy the necessary condition (5.309)

1

For all parameters g(x) looks qualitatively like the function shown in Fig. 5.30 because for κ ˜ > 0 it follows that g(x + π/2) ≤ g(x) for x ∈ [0, π/2] and |g(x − π/2)| ≤ |g(x)| for x ∈ [−π/2, 0].

182


Saddle Node and Pitchfork Bifurcation Let us exploit the results obtained so far in order to generalize the bifurcation diagram shown in Fig. 5.28a) to the case in which the symmetry constraint (5.288) does not hold. Substituting (5.285) for θst = π into (5.307), we obtain λθst =π =

α ˜ |rst | − 4β˜ cos(2x)P˜st (x;θst =π) . 1 − 2π P˜st (0; θst = π)

(5.316)

For vanishing noise, we have rst = 1 and, following the preceding reasoning, ˜ which is the Lyapunov exponent derived from the we obtain λθst =π = α ˜ − 4β, linear stability analysis of the stationary point qst = π of the deterministic HKB model (5.283). Equation (5.316) was evaluated numerically using the potential (5.297) rather than (5.282). Figure 5.29a shows two surfaces dividing the parameter space (˜ κ, α ˜ , e) into two regions. The “roof-like” surface was adopted from Fig. 5.28a and marks the critical points at which the stationary solutions with θst = π cease to exist (saddle node bifurcation points). The “wall-like” surface separates the region in which the stationary probability ˜ 1 > 0 yields, according to (5.316), λθ =π < 0 (to density with θst = π and λ st the right of the wall-like surface) and the region in which the stationary probability density yields λθst =π > 0 (to the left of the wall-like surface). From our previous analysis we conclude that the “wall-like” surface in Fig. 5.29a describes points related to a pitchfork bifurcation. In sum, within the cuboid subspace that is shaped by the two surfaces an asymptotically stable stationary probability density with θst ≡ π exists. Outside this subspace, the stationary probability densities with θst = π are either unstable or entirely absent. In contrast, the stationary probability density with θst = 0 describes an asymptotically stable solution in the whole parameter space (˜ κ, α ˜ , e) for ˜ for α α ˜ > 0, κ ˜ ≥ 0, e ≥ 0 (or equivalently in the space (˜ κ, α ˜ , β) ˜ > 0, κ ˜ ≥ 0, β˜ ≥ 0). Finally, Fig. 5.29d shows the result of a simulation of the mean field HKB model (5.284) with β˜ = α ˜ e/4, where the parameter e was varied along the dashed line depicted in Fig. 5.29b. That is, we use κ ˜ = 4 and α ˜ = 0.5. A simulation scheme was used as described above in the context of the saddle node bifurcation of the cluster amplitude. However, this time the imaginary parts of the time-dependent coefficients were included. The noisy Gaussian probability density shown in panel d) served as the initial distribution. The parameter e was decreased in steps of 0.1 from 1.8 to 1.4 after each computation of 106 single time steps. In agreement with the results obtained from the linear stability analysis shown in panel b) and in accordance with the branching of solutions in the bifurcation diagram shown in panel c), the phase transition occurred at a critical value of about ec = 1.6.

5.4 Characteristics of Bifurcations

183

5.4 Characteristics of Bifurcations 5.4.1 Stability and Disorder There is a close relationship between the disorder and the stability of stationary distributions of nonlinear Fokker–Planck equations when disorder is measured in terms of the variance and similar statistical measures. Accordingly, states with a large degree of order are described by distributions with small variances, whereas states with a large degree of disorder are described by distributions with larger variances. Since the free energy of the Desai– Zwanzig model reads κ F = UL + K − Q BS (5.317) 2 (see (5.184)), we find that the smaller K, the smaller the free energy F . That is, the free energy is low for states with a small degree of disorder. In the case of the KSS model and the mean field HKB model, the disorder can be measured in terms of the cluster amplitude r. For unimodal distributions large values of r correspond to states of high order (low disorder), whereas small values of r are related to states of low order (large disorder), see Sect. 5.3.1. Since we have r ∈ [0, 1], we may say that for unimodal distributions small values of 1 − r correspond to states of high order, whereas large values of 1 − r describe states of low order. The free energies of the KSS model and the mean field HKB model read κ F = − r2 − Q BS , 2 κ F = UL − r2 − Q BS 2

(5.318)

(see (5.233) and (5.278)). We find that the larger r (i.e., the smaller 1−r), the smaller F . Roughly speaking, this implies that the free energies are smaller for ordered states than for disordered states – just as in the case of the Desai– Zwanzig model. Since we study systems that converge to states of minimal free energy, a naive but useful notion is that stable states are related to states with minimal disorder. In fact, as shown in Fig. 5.31, in the multistable regime states with a relatively high degree of order are stable, whereas states with a relatively high degree of disorder are unstable ones. The diagram for the Desai–Zwanzig model shown in Fig. 5.31 can be deduced from (5.63). Equation (5.63) states that for fixed control parameters κ and Q the expression dR/dm is proportional to the variance K of the stationary distributions. Since we have dR/dm > 1 for unstable distributions and dR/dm < 1 for stable distributions, it follows that in the bistable regime the variance of stable solutions is smaller than the variance of unstable solutions. Note that for all KA -models we can obtain a similar result: in the multistable regime stable stationary solutions have smaller KA -values than unstable stationary solutions. The reason for

184


DZ model

K

KSS model (sine−coupling)

MF−HKB model

1−r

(s)

1−r (s)

(u)

(u)

(u) (s)

(s)

(s)

(s)

κ

κ

κ

Q

Q

Q

Fig. 5.31. Stability and degree of disorder of the stationary distributions of three mean field models: the Desai–Zwanzig model, the KSS model with a sine couplingforce, and the mean field HKB model; (u) and (s) denote unstable and stable distributions

this is that for the KA -model (5.76) the relation (5.80) holds. The diagram for the KSS model corresponds to Fig. 5.25. The diagram for the mean field HKB model shows only the symmetric stationary solutions and can be read off from panel c) in Fig. 5.28. There we see that at the saddle node bifurcation point (graph II) the signed cluster amplitude ru of the unstable stationary solution is equivalent to the cluster amplitude rs of the stable stationary solution with rs < 0, whereas in the multistable regime (graph I) ru lies closer to zero than rs , which implies that the original cluster amplitudes ru = −ru and rs = −rs satisfy the relation rs > ru . In sum, for the aforementioned models there are two stability criteria. First, stable distributions correspond to free energy minima, whereas unstable distributions correspond to free energy maxima or saddle points. Second, in the multistable regime unstable distributions correspond to states of large disorder, whereas stable distributions correspond to states of small disorder, when disorder is measured in terms of the variance of distributions or similar statistical quantities. 5.4.2 Emergence of Collective Behavior (1)

The bifurcation from a stationary distribution Pst to a stationary distribu(2) tion Pst can often be interpreted as the emergence of a collective behavior in a many-body system or the change between different kinds of collective behavior. To this end, it is assumed that the solutions of nonlinear Fokker– Planck equations describe the distributions of subsystems of many-body systems (µ-space description, see Sect. 1.1.2). For example, let us consider the Desai–Zwanzig model in the parameter range in which it exhibits unimodal


κ

185

Q Q

κ

DZ model P

P

x

P

x

KSS model

P

P

P

x

x

x P

x

x MF−HKB model P

P

P

x

x

x

Fig. 5.32. Number and shape of the stable stationary distributions of three mean field models (Desai–Zwanzig model, KSS model, and mean field HKB model) in two different parameter regimes: κ Q (left column) and κ Q (right column)

stationary distributions only. Then, the symmetric stationary distribution (1) Pst of the Desai–Zwanzig model is given by a bell-shaped distribution with vanishing mean value that describes a many-body system with subsystems without any preference or collective behavior. The asymmetric stationary (2) distributions Pst describe subsystems that assume on the average positive (or negative) state values and in this sense they describe subsystems that exhibit a common tendency or a collective behavior, see Fig. 5.32. Likewise, (1) the uniform distribution Pst of the KSS model with sine coupling-force describes a many-body system that does not exhibit any collective behavior. (1) In contrast, unimodal distributions Pst of the KSS model describe subsystems that are centered around the cluster phase θst (see also Sect. 5.3.1) and

186


in this sense show a collective behavior. Finally, let us consider the HKB model in the parameter range where it exhibits unimodal stationary distri˜ the butions. In this case, for κ ˜ = κ/Q < κ ˜ c and fixed values of α ˜ and β, (1) mean field HKB model exhibits a unique stationary distribution Pst with a single peak at x = 0. However, if κ ˜ exceeds a critical value κ ˜ c there is another asymptotically stable, unimodal distribution that exhibits a peak at x = π. Consequently, if the model is prepared in a parameter regime with κ ˜ > κ ˜ c and subsequently parameters are changed such that the model becomes monostable (i.e., κ ˜ → κ ˜ < κ ˜ c ), then we observe a phase transition between two different kinds of collective behavior. 5.4.3 Multistability and Symmetry Multistabilities often arise due to symmetries of many-body systems. Let us illustrate this relationship by means of a few examples. A many-body system related to the Desai–Zwanzig model discussed in Sect. 5.2.3 may be defined by means of the multivariate Langevin N0 d κ (Xi − Xk ) + Q Γi (t) , Xi (t) = aXi − bXi3 − N0 dt

(5.319)

k=1

with i = 1, . . . , N0 . In fact, in the limit N0 → ∞ we may replace the subsystem ensemble {X1 , . . . , XN0 } in the interaction term by means of a statistical ensemble {X 1 , . . . , X N } of a single subsystem and thus obtain the Desai– Zwanzig model (see Sect. 3.8). The many-body system defined by (5.319) is invariant under the inversion defined by Xi → −Xi . On account of this inversion symmetry, we conclude that if the many-body system exhibits a collective behavior N0 in terms of a phase with a nonvanishing order parameter q = N −1 k=1 Xk , then this collective behavior comes in two types: one type with q > 0 and another one with q < 0. The situation is reminiscent of the behavior of an Ising ferromagnet, where in the ferromagnetic phase the spins preferably point up or point down (see Sec. 5.5.1). The inversion symmetry of the many-body system described by (5.319) carries over to the Desai–Zwanzig model (5.180). The nonlinear Fokker–Planck equation (5.180) is invariant under inversion x → −x. Therefore, as shown in Fig. 5.32 in the strong coupling regime (i.e. for κ Q) there is not only one asymmetric stationary distribution but there are two of them. A many-body system related to the KSS model with sine coupling-force (see Sect. 5.3.2) is given by N0 d κ Xi (t) = − sin(Xi − Xk ) + Q Γi (t) , N0 dt

(5.320)

k=1

with i = 1, . . . , N0 . The many-body system is invariant under translations defined by Xi → Xi + ∆x. Consequently, if there is a collective behavior with a


187

N0 nonvanishing cluster amplitude r = |N0−1 k=1 exp{iXk }| then there are infinite many types of this collective behavior. The situation here is reminiscent of a planar rotator ferromagnet, where the magnetization in the ferromagnetic phase can point in any direction of the XY -plane (see Sect. 5.5.1). The translation symmetry of the many-body system given by (5.320) can also be found in the KSS model (5.229). Therefore, as pointed out in Sect. 5.3.2 and as shown in Fig. 5.32 in the strong coupling regime (i.e. for κ Q) there is a continuous family of stationary distributions. The mean field HKB model (5.260) for vanishing α-term is invariant under the operation x → x + π. Therefore, as shown in Fig. 5.32 in the strong coupling regime (i.e. for κ Q) there are two stationary distributions. The α-term breaks the symmetry property of the mean field HKB model for α = 0, which is the reason why for α > 0 and weak coupling (i.e. for κ Q) only one distribution survives (see Fig. 5.32 again). 5.4.4 Continuous and Discontinuous Phase Transitions We refer to phase transitions of the solutions of mean field models as continuous if the order parameters of the models change continuously at phase transition points. In other words, if we regard the stationary order parameter values Mst of a mean field model as a function of a control parameter α, Mst = Mst (α), and if Mst is a continuous function of α at a phase transition point αc , then the phase transition is a continuous one. If there is a discontinuous change (i.e., if Mst (α) “jumps” from one value to another) then we are dealing with a discontinuous phase transition. For example, the Desai–Zwanzig model exhibits a continuous phase transition. As shown in the bifurcation diagrams 5.19 and 5.20 the order parameter Xst changes continuously at the phase transition point. In contrast, the mean field HKB model exhibits a discontinuous phase transition. As shown in the bifurcation diagram 5.29c and in Figs. 5.28d and 5.29d the cluster phase θst changes discontinuously from π to zero. Some models and the type of phase transition they exhibit are listed in Table 5.3. The liquid crystal model will be discussed in Sect. 5.5.3. Table 5.3. Some mean field models and the type of bifurcations that they describe Continuous phase transitions

dynamical Takatsuji model Desai–Zwanzig model bounded B(M1 ) model with double-well potential B(z) KSS model with sine coupling-force

Discontinuous phase transitions

mean field HKB model liquid crystal model

188


5.5 Applications 5.5.1 Ferromagnetism Ferromagnetic materials exhibit a magnetization at temperatures below a critical temperature Tc . For temperatures larger than Tc this magnetization vanishes. That is, there is a phase transition between two phases: a ferromagnetic phase (finite magnetization) and a paramagnetic phase (no magnetization). The reason for this behavior is that ferromagnetic materials are composed of a large number of interacting elementary magnets given by atomic spins. The exchange energy between pairs of spins is lower for parallel spin orientations than for anti-parallel spin orientations [11, 89, 229, 490, 546, 579]. Consequently, spin-spin interactions tend to establish a highly ordered state with all spins in parallel. The spins exchange heat energy with their environment, which leads to a thermal motion of the spins. The thermal motion of the spins tends to establish random spin orientations. In sum, if thermal spin fluctuations dominate, the overall magnetization vanishes and ferromagnetic materials are in the paramagnetic phase, whereas if spin-spin interactions dominate, spins align themselves into a state with parallel orientations and, as a result, there is a non-vanishing magnetization and ferromagnets are in their ferromagnetic phases, see Fig. 5.33.

T > Tc

T < Tc

paramagnetic phase

ferromagnetic phase

isotropic phase

nematic phase

Fig. 5.33. Ordered and disordered states of ferromagnetic materials (upper panels) and liquid crystals (lower panels)

Spins can be described by three-dimensional vectors s = (sx , sy , sz ) subjected to the constraint |s| = S (note that S does not denote an entropy mea-

5.5 Applications

189

sure here). The components sx , sy , sz play different roles for different kinds of ferromagnetic materials. In some materials only the z-components of spins are involved in spin-spin interactions. Materials of this kind are referred to as Ising ferromagnets. For Ising ferromagnets the magnetization Mz points along the z-axis and is given by Mz = sz , where the average is carried out with respect to the ensemble of spins. For T > Tc we have Mz = sz = 0. For T < Tc the spins point on the average either in the direction of the z-axis (Mz = sz > 0) or in the opposite direction (Mz = sz < 0). That is, for T > Tc the system is monostable, whereas for T < Tc it is bistable. In other ferromagnetic materials spins are predominantly affected by spin-spin interactions within a plane, the so-called “easy plane” or XY -plane. Materials of this kind exhibit spin-spin coupling forces involving the components sx and sy . We will refer to materials with easy planes as XY -ferromagnets. Soft-spin Ising Ferromagnets and the Desai–Zwanzig Model Let us consider an ensemble of N0 spins and describe the components sz of the spins by means of the state variables Xk for k = 1, . . . , N0 . Furthermore, let us regard the fluctuation strength Q as a temperature measure T and consider the first moment M1 = N0−1 k Xk as a measure for the magnetization Mz . Then, if we neglect correlations between subsystems and identify the state variables Xk with the statistically-independent realization X k of a random variable X ∈ Ω = lR, we arrive at mean field models for the one-dimensional Ising ferromagnet. In Sect. 5.2.2 we have already elucidated the relationship between the dynamical Takatsuji model and the Ising ferromagnet. Now, let us focus on the Desai–Zwanzig model. If we regard the Desai–Zwanzig model as a model for a one-dimensional Ising ferromagnet, then the bifurcation diagram depicted in Fig. 5.20 may be regarded as the bifurcation diagram of an Ising ferromagnet. Moreover, since the Desai–Zwanzig model is a nonlinear Fokker– Planck equation and the nonlinearities of nonlinear Fokker–Planck equations are assumed to reflect subsystem-subsystem interactions, the Desai–Zwanzig model indeed accounts for the mechanism that leads to the ferromagnetic phase, namely, the interactions between spins. As shown in Fig. 5.32, the ferromagnetic phases exist when spin-spin interactions dominate fluctuations, whereas the paramagnetic phase exists when fluctuations dominate the spinspin interactions (which is in line with Fig. 5.33 when we put Q = T ). Finally, we would like to point out that we are dealing with a soft-spin model [143] because in contrast to the spin variables that are subjected to the constraint |s| = S, the random variables Xk are not subjected to such a constraint. However, on account of the potential V (x)= −ax2 /2 + bx4 /4 the variables Xk are attracted to the positions x1,2 = ± 2a/b that describe the potential minima. That is, the Desai–Zwanzig model involves a weak (or soft) version of the constraint to which spin variables are subjected (whence the name soft-spin model).

190


Planar Rotator Ferromagnets and the KSS Model There are two kinds of models for XY -ferromagnets: planar rotator models and XY -models. In the case of planar rotator models, the three-dimensional spin vectors are confined to the XY -plane and therefore, can be described in terms of a single angular variable X ∈ Ω = [0, 2π]. More precisely, we have sz = 0 and s = (sx , sy ) = (cos X, sin X) [307, 318, 331, 345, 407]. Note that this representation implies that |s| = S = 1. In contrast, the XY model describes ferromagnet materials with spins that can have a nonvanishing z-component [234, 417, 548]. The KSS model with sine coupling-force and the mean field HKB model can be regarded as planar rotator models for ferromagnets with infinite-range spin-spin interactions [172, 199, 603]. In the case of infinite-range interactions [546], there is an all-to-all coupling between the spins. the interaction NConsequently, N0 energy Hss is given 0 cos(Xi − Xk ) with by Hss = −0.5κN0−1 i,k=1 si · sk = −0.5κN0−1 i,k=1 sn = (cos Xn , sin Xn ). Here, κ > 0 is a proportional factor used to compute N0 the energy Ei of a single spin i in the mean field S = N0−1 k=1 sk like N0 Ei = −κsi · S. In the sum i,k=1 si · sk the exchange energy of each spin-pair is counted twice. Therefore, we have introduced in Hss the factor 0.5. Taking external magnetic fields and other symmetry breaking (crystalline) fields N0 into account, we obtain additional Hamiltonians such as i=1 cos(Xi ) (magN0 N0 netic fields), i=1 cos(2Xi ) (uniaxial anisotropies), and i=1 cos(nXi ) (nfold anisotropies) [229, 316, 406, 611]. For example, a constant magnetic field given by f = (1, 0) gives rise to the interaction energies f ·si = cos Xi . Furthermore, if an anisotropy of an XY -ferromagnet can be described by means of a 2 × 2-matrix A with matrix elements A1,1 = −A2,2 = 1 and A1,2 = A2,1 = 0, then the potential energy of a spin si = (cos Xi , sin Xi ) with respect to this anisotropy is given by si · A · si = cos(2Xi ). In sum, the total Hamiltonian of a planar rotator model with infinite-range interactions and symmetry breakN N0 ing fields reads Htot = −κN0−1 i,k0 cos(Xi − Xk ) − n cn i=1 cos(nXi ), where the parameters cn denote coupling factors. Taking fluctuating forces into account, we may describe the stochastic behavior of the coupled planar rotators by means of the multivariate Langevin equation d ∂ Htot + Q Γi (t) . (5.321) Xi (t) = − dt ∂Xi If at time t = t0 the random variables Xi are statistically-independent and described by the same distribution u(x), then in the limit N0 → ∞ the random variables Xk correspond to the realizations X k of a random variable X and (5.321) becomes d cn sin(nX) − κ sin(X − X ) + Q Γ (t) , (5.322) X(t) = − dt n see Sect. 3.8. The stochastic process given by X(t) can then equivalently be described in terms of the free energy Fokker–Planck equation

5.5 Applications

6

191

7

∂2 ∂ ∂ sin(x−x )P (x , t; u) dx P +Q 2 P cn sin(nx) + κ P (x, t; u) = ∂x ∂t ∂x n Ω (5.323) and the evolution equation ∂ P (x, t|x , t ; u) = ∂t 6 7

∂ cn sin(nx) + κ sin(x − x )P (x , t; u) dx P (x, t|x , t ; u) ∂x n Ω +Q

∂2 P (x, t|x , t ; u) . ∂x2

(5.324)

Equation (5.323) reduces to the KSS model with sine coupling-force for cn≥0 = 0 and the mean field HKB model for c1 = α, c2 = β, and cn≥3 = 0. According to this approach to ferromagnetic materials, the nonuniform stationary solutions of the KSS model describe ferromagnetic phases of planar rotator ferromagnets, whereas the uniform solution describes paramagnetic phases. In order to take the impact of the symmetry breaking field into account, we would need to supplement the KSS model with pinning forces. That is, we would need to consider models such as the mean field HKB model. 5.5.2 Synchronization There are numerous examples of many-body systems with subsystems that exhibit synchronized oscillatory behavior. In particular, there are various biological and social systems showing behavioral synchronization and there are many examples of synchronized neural activity. Let us mention a few of them. Applause The applause after a concert is a typical example for mass-behavior of humans. Applause usually exhibits the following two states pattern. There is an initial period in which people clap with their preferred frequencies and, thus, produce an unsynchronized applause. Subsequently, the audience finds a common clapping frequency. During this second period, not only are individuals entrained by the common clapping frequency, they also perform their clapping movements with roughly the same phase angles [441]. In view of these characteristics, the unsynchronized and synchronized applause can be distinguished using a mean harmonic correlation function introduced in [441], which reflects a collective property of applause. More precisely, the correlations between the signals of the members of an audience and a harmonic function with fixed frequency and phase are computed and averaged. Frequency and phase of the harmonic function are adjusted in order to obtain a

192


maximum value. Unsynchronized applause produces low values irrespective of the parameter values for frequency and phase. In contrast, synchronized applause yields large function values. By comparing the clapping behavior of isolated individuals with the clapping behavior of individual members of audiences, one can show that the clapping behavior changes due to the acoustic interactions between individuals [441]. In short, in this example acoustic coupling forces result in the emergence of a collective synchronized behavior. Tree Crickets and Fireflies Snowy tree crickets chirp in a rhythmic pattern with frequencies between 50 and 200 chirps per minute depending on the temperature of their environments [616]. With their tympanic organs (receptors for acoustic stimuli) removed, they chirp with individual phase lags. Consequently, populations of these crickets produce de-synchronized chirping patterns [616]. In contrast, populations of intact snowy tree crickets are known to chirp in unison. That is, these crickets usually synchronize their chirping behavior [616]. To this end, a cricket shortens the interval between two consecutive chirps if its chirping call follows the calls of other crickets such that the subsequent call is closer to the calls of the other crickets. Likewise, a cricket lengthens a chirp interval if its own call is ahead of the calls of other crickets [616, 633]. In view of these observations, it has been suggested that cricket populations feature a collective behavior, namely, they form choruses producing synchronized calling songs [557, 633]. The formation of choruses can be regarded as a process of self-organization that is established by means of acoustic couplings between the individuals. In the absence of these couplings there is no chorusing. In contrast, if the coupling forces dominate, then synchronized behavior can emerge. The emergence of the collective behavior can be described by means of the non-uniformity of the phase distribution of cricket chirps. The degree of non-uniformity can easily be quantified in terms of the cluster amplitude r, see Sect. 5.3.1. Unsynchronized chirping corresponds to a uniform phase distribution and a vanishing degree of non-uniformity (i.e., r = 0), whereas chorusing and synchronized chirping involves a nonuniform phase distribution (i.e., r > 0). It is known that some fireflies flash in isolation with rhythmic patterns at frequencies in the range from 1 to 2 Hz. When a population of these fireflies is put together, for example, on a tree, then the fireflies flash with a common frequency and almost vanishing phase differences, that is, the population exhibits a communal synchronized flashing [81]. It has been observed that the fireflies are entrained by the flashes of their fellow-fireflies. In response to flash-like stimuli, a firefly shortens or lengthens the intervals between its consecutive flashes such that its own flashing pattern approaches the stimulus pattern [82, 277, 633]. Therefore, it is generally assumed that the synchronous flashing of firefly populations results from self-organization and the visual couplings between the population members. The establishment of

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a communal synchronous rhythm can quantitatively be assessed in terms of the non-uniformity or the cluster amplitude r of firefly flashes. Just as in the previous examples, fireflies that do not synchronize their flashings produce a uniform phase distribution with a vanishing degree of non-uniformity (i.e., we have r = 0), whereas fireflies that synchronize their flashings produce a unimodal phase distribution with a finite degree of non-uniformity (i.e., we have r > 0). Synchronization of Brain Activity An important concept in neuroscience is that the neocortex of humans and animals is organized as a map. Particular areas correspond to functional abilities (e.g., memory) and sensory and motoric organs (see e.g. [578]). We may regard these areas as “black boxes”, neural dipoles, or elementary neural units and describe their functioning by means of zero-dimensional models (just as we would describe the functioning of an Ohmic resistance). According to a new paradigm in neuroscience, however, neural computation involves the cooperative activity of many spatially distributed neurons. In particular, it is believed that perception and action involve spatially extended systems composed of many neurons that are bound to task-related entities by synchronizing their activity. Using cross-correlation analysis, in animal studies with cats, synchronized neural activity has been found in functional columns of the visual cortex [239, 538], among several unilateral areas of the visual cortex [150], and between left- and right-hemispheric visual areas [151]. Although synchronization typically occurs during the presentation of an object, it is assumed that the visual stimulus does not act as a driving force in order to establish a population of synchronized neurons. On the basis of theoretical reasoning and experimental evidence, it has been suggested that synchronization emerges due to mutual couplings between so-called neural oscillators. Accordingly, the synchronization of particular populations of neurons corresponds to particular perceptions [122, 539, 614]. Moreover, if in animal experiments the corticocortical connections between cortical hemispheres are removed, then synchronization between the hemispheres vanishes despite of the presence of a visual stimulus [151]. Synchronized oscillatory neural activity has also been found during the performance of manual tasks. There are significant cross-correlations between neural populations of different unilateral cortical regions when monkeys perform perceptual-motor tasks [75]. Such correlations are almost entirely absent before and after task performance. In similar animal studies, it has been found that arm movements involve both uni- and bilateral synchronized brain activity [439]. Synchronized brain activity has also been found in man. For example, it has been shown that visual flicker signals can induce synchronized oscillatory neural activity over the whole cortex [537]. In addition, it has been shown that synchronization between different cortical areas occurs

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during tremor [567, 566], the production of isometric forces [245], and when humans listen to music [56]. The conflict between zero-dimensional and spatially distributed neural units is a conflict between localized and nonlocalized task-related neural activity. Probably the truth is to be found somewhere in between these extremes. In order to illustrate this, we may compare the situation with the theories of electromagnetism and gravity. Both theories deal with localized, zero-dimensional elements (charged particles and particles with mass, respectively) as well as nonlocalized, spatially extended elements (electromagnetic fields and gravitational fields, respectively). There are problems that can be treated solely by reference to the localized elements. Other problems only involve the field theoretical aspects of electromagnetism and gravity. Similarly, a comprehensive account of neural task-related activity may combine zero-dimensional and spatially distributed task-related units. Nevertheless, in special cases it may be sufficient to model neural systems as either zerodimensional or spatially extended systems. In the latter case, mean field models such as the KSS model and extensions of it are tailored to describe the synchronization of neural activity produced by populations of neurons and neuronal units. Synchronization, Planar Rotators and Phase Oscillators The KSS model and modifications of it have frequently been used to describe the emergence of synchronized states of neural activity. The reason for this is that it often seems sufficient to describe ensembles of oscillatory constituents by means of coupled planar rotators in order to obtain a good understanding of the observed phenomenon. In the context of neural activity, one often refers to planar rotators as phase oscillators. The state Yi (t) of a phase oscillator is given by Yi (t) = A sin(ωt + Xi (t)) . (5.325) Here, A and ω are amplitude and frequency of the oscillator and assume fixed values. We realize that the temporal evolution of a phase oscillator is completely described by the phase Xi . Let us label the ensemble members by i = 1, 2, . . .. Then, it is clear from (5.325) that in this simple case all phase oscillators have the same amplitude and eigenfrequency. Moreover, the oscillator ensemble is completely de-synchronized if the phases Xi are uniformly distributed. If the distribution of Xi differs from the uniform distribution, then there is a partial synchronization of the oscillator ensemble. If we neglect statistical correlations between the oscillators, we can describe the states Xi by means of the realizations X i of the random variable X defined by the KSS model. Then, the synchronized states emerge when the uniform stationary distribution of the KSS model becomes unstable and gives rise to a stable stationary non-uniform distribution.

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Bibliographic Note Our understanding of how synchronization can emerge in coupled oscillator systems of the mean field type was in particular advanced by studies of Winfree [632, 633] and Kuramoto [365]. Synchronization in the context of nonlinear Fokker–Planck equations has been extensively studied in the literature. The reader may consult the review articles and monographs [477, 552, 557, 568]. For further information on this topic see also Sect. 7.5. 5.5.3 Isotropic-nematic Phase Transitions and Maier–Saupe Model Liquid crystals combine properties of solids and liquids. They can exhibit both some kind of microscopic order (just as in solids) and fluidity (just as in liquids) [129, 131]. Liquid crystals can exhibit an isotropic and a nematic phase. In the isotropic phase the orientations of the molecules are randomly distributed, whereas in the nematic phase all molecules point in roughly the same direction, see Fig. 5.33. The isotropic phase can be regarded as a state of orientational disorder, whereas the nematic phase exhibits orientational order. The degree of alignment of the molecules is a statistical measure that describes how the orientations of the molecules are distributed and can be regarded as an order parameter q. If the molecules’ orientations are uniformly distributed (isotropic phase), then there is no alignment and, consequently, we put the degree of alignment equal to zero (i.e., we have q = 0). If all molecules point in exactly the same direction, the degree of alignment becomes unity (i.e., we have q = 1). The order-disorder phase transition from the isotropic phase to the nematic phase involves the emergence of a collective (or cooperative) behavior: the alignment of molecules. That is, the isotropicnematic phase transition can be described in terms of q by means of a change from q = 0 to q > 0 [90, 129]. The alignment of molecules is an example of self-organization because it is caused by the interaction forces between the molecules of a liquid crystal. The molecules themselves produce an overall torque force that can be described, for example, in terms of the Maier–Saupe potential (see below). This torque force acts back on the individual molecules and tends to establish a nematic phase. If fluctuating forces dominate, then the overall torque force cannot be established and, consequently, the crystal settles down in the isotropic phase. In contrast, if the interaction forces dominate, the collective torque force emerges and results in an alignment of the molecules and the emergence of a nematic phase. The orientation of a simple macromolecule can be described by means of a director n = (nx , ny , nz ) ∈ Ω. The director is normalized to unity |n| = 1, which implies that nx , ny , nz ∈ [−1, 1] and that there are only two free parameters at our disposal. This becomes obvious if n is given in spherical polar coordinates: n = (sin ϑ sin ϕ, sin ϑ cos ϕ, cos ϑ) with ϑ ∈ [0, π] and ϕ ∈ [0, 2π].

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Accordingly, the phase space Ω of n is the surface of a sphere with radius 1. Orientational order can be described by means of the order parameter 5 1 1 3 cos2 (ϑ) − 1 P (n) = (3 cos2 (ϑ) − 1)P (n)dO (5.326) q = A(ϑ) = 2 2 Ω defined as the mean value of A(ϑ) = [3 cos2 (ϑ) − 1]/2 [90, 129, 485, 551]. In order to elucidate the role of the order parameter q, let us consider liquid crystals with a rotational symmetry around an axis, say, the z-axis. Then, ϕ is uniformly distributed: P (ϕ) = 1/(2π). In this case the statistical properties of liquid crystals are primarily described by the director distribution P (nz ) with nz ∈ Ωz = [−1, 1]. For macromolecules with rotational symmetry the order parameter q becomes

1 1 (3n2z − 1)P (nz )dnz . (5.327) q= 2 −1 We assume that the director is a non-polar vector, which means that a macromolecule with n∗ has the same properties as a molecule with −n∗ . In this case, director distributions P (nz ) are symmetric with respect to the origin: P (nz ) = P (−nz ). In the isotropic phase the director components nz are uniformly distributed in [−1, 1], that is, we have P (nz ) = 1/2. Consequently, for the isotropic phase we obtain q = 0. Note that the distribution P (ϑ) of the isotropic phase is not uniform because the transformation nz = cos(ϑ) yields P (nz ) = 1/2 ⇒ P (ϑ) = sin(ϑ)/2 (for the transformation of random variables see e.g. [498]). If P (nz ) differs from the uniform distribution, we have orientational order to a certain extent and refer to the phase as nematic. We choose our coordinate system in such a way that in the nematic phase the directors have the tendency to be parallel to the z-axis. Then, in the nematic phase we have q > 0. As a result, the emergence of the nematic phase from the isotropic phase goes along with a bifurcation of q from q = 0 to q > 0 – as mentioned previously. If there is a complete alignment of the molecules, we have only molecules with nz = 1 and nz = −1. The corresponding probability distribution is P (nz ) = [δ(nz − 1) + δ(nz + 1)]/2 and the order parameter assumes its maximum value: q = 1. Maier–Saupe Mean Field Theory We consider here liquid crystals to which the Maier–Saupe theory applies [90, 129, 399, 400, 485, 551]. The macromolecules are assumed to interact with each other by means of electronic dipole forces. The strength of the dipole-dipole interactions depends on the orientations of the molecules. The interaction energy between one macromolecule and all other macromolecules depends, roughly speaking, on the orientation of the macromolecule with respect to the mean orientation of all other molecules and is given

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by Ei = −κA(ϑi ) A(ϑ). Consequently, the total interaction energy reads U = −κq 2 /2. Likewise, the free energy is given by κ F [P (n)] = − q 2 − T orS[P (n)] , (5.328) 2 where orS[P (n)] denotes the orientational entropy defined by [485] 5 or P [n(ϕ, θ)] ln P [n(ϕ, θ)] dO S[P ] = − Ω 2π

=−

dϕ

0

π

dθ sin(θ)P [n(ϕ, θ)] ln P [n(ϕ, θ)] .

(5.329)

0

Assuming now rotational symmetry of the macromolecules and using X = nz , we obtain κ F [P ] = − q 2 − T BS[P ] 2 κ 2 = − A − T BS[P ] (5.330) 2 with q = A, BS[P ] = − Ωz P ln P dx, and 3x2 − 1 . (5.331) 2 The free energy (5.330) belongs to the class of free energies given by (5.317) and (5.318). The free energy Fokker–Planck equation (5.3) can be found as 1 ∂ ∂2 9 ∂ P (x, t; u) = − κ x X 2 − P + T 2P . (5.332) ∂t 2 ∂x 3 ∂x A(x) =

Note that X = 1 (ϑ = 0) is equivalent to X = −1 (ϑ = π) because (as mentioned earlier) a director n∗ is equivalent to a director −n∗ that points in the opposite direction. Consequently, we study solutions of (5.332) that are defined on x ∈ [−1, 1] and satisfy both periodic boundary conditions and the additional constraint that P (x) is a symmetric function. In view of these considerations, one may say that the whole physics of the liquid crystal model is given by a random walk defined on [0, 1] with reflective boundaries at x = 0 and x = 1. However, in what follows, for the sake of convenience, we will continue to use X defined on [−1, 1]. For appropriate initial distributions u(x) the second moment X 2 will correspond to a continuous nonsingular function with respect to t. For such initial distributions the evolution equation (5.332) is a strongly nonlinear Fokker–Planck equation and Markov diffusion processes can be defined by means of the solutions of (5.332) and the evolution equation ∂ P (x, t|x , t ; u) = ∂t 2 1 ∂2 9 ∂ P (x, t|x , t ; u) + T 2 P (x, t|x , t ; u) − κ x X P (x,t;u) − 2 ∂x 3 ∂x (5.333)

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or, alternatively, in terms of the Langevin equation √ 1 d 9 + T Γ (t) . X(t) = κX X 2 − dt 2 3

(5.334)

Equation (5.332) can be regarded as a special case of the generic model (5.107) for U0 = 0, d = 1, κ1 = κ, and T = Q. Consequently, stationary solutions of (5.332) can be obtained from (5.109) and are given by A(x) Ast 1 Pst (x) = exp κ Z T 2 3κx (3X 2 − 1)/2 st 1 . (5.335) = exp Z 2T The order parameter qst = Ast corresponds to solutions of the selfconsistency equation m = R(m) defined by 3κx2 m 1 exp , (5.336) P (x, m) = Z (m) 2T

1 3κx2 m Z (m) = dx (5.337) exp 2T −1 and

1

R(m) = −1

3x2 − 1 P (x, m) dx , 2

(5.338)

see also (5.110) and (5.111). Stationary Solutions and Stability Analysis Since we are dealing with the special case d = 1, the stability matrix given by (5.104) and (5.106) of the generic model (5.107) reduces to the stability ˜ = Q+KA,st d2 B/dm2 , see Table 5.1 coefficient of the model (5.83), which is λ (third column). In our case we have B(z) = −κz 2 /2 and Q = T , which leads ˜ = T − κKA,st . Consequently, the stability of the stationary distributions to λ ˜ with can be read off from the sign of λ KA,st =

2 2 1 1 (3X 2 − 1)2 st − (3X 2 − 1) st . 4

(5.339)

We realize that m = 0 is a solution of the self-consistency equation R(m) = m for all ratios κ/T . From m = 0 it follows that Pst = 1/2 and KA,st = 1/5, ˜ = T − κ/5. Consequently, which, in turn, gives us the stability coefficient λ the isotropic phase is asymptotically stable for T > κ/5. Conversely, the isotropic phase is unstable for T < κ/5. In order to study the emergence

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199

0.1 0.08 R’(m)

0.06 0.04 0.02

0 –0.02

0.1

0.2

0.3

m

0.4

0.6

0.5

0.7

–0.04 –0.06 –0.08 –0.1

Fig. 5.34. Illustration of the self-consistency equation R (m) = R(m) − m = 0 (see (5.340)). Zeros of R (m) correspond to stationary distributions; dR (m)/dm < 0 (> 0) at R (m) = 0 describe asymptotically stable (unstable) stationary distributions. From bottom to top: T /κ = 0.3, T /κ ≈ 0.223 (saddle node bifurcation point; emergence of the nematic phase), T /κ = 0.21, and T /κ = 1/5 (the isotropic phase becomes unstable)

q

1 0.8 0.6 0.4 0.2 0

2

4

6

8

κ

10

Fig. 5.35. Bifurcation diagram of the order parameter q of the Maier–Saupe model obtained from the self-consistency equation R (q) = R(q) − q = 0 (solid line). Only stable stationary solutions are shown. The upper branch of the bifurcation diagram was also determined by solving numerically the Langevin equation (5.334) using the averaging method for self-consistent Langevin equations and periodic boundary conditions for X ∈ [−1, 1] (diamonds). Parameters: T = 1 (L = 50000, ∆t = 10−4 , wn via Box-Muller, initial distribution u(x) = [δ(x − 0.8) + δ(x + 0.8)]/2, κ was gradually increased in steps of 0.5 starting with κ = 5.0)

of the nematic phase, we evaluate numerically the self-consistency equation m = R(m) in the form of R (m) = R(m) − m = 0 .

(5.340)

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It is clear from our discussion of the bounded potential model (5.83) that solutions R (m) = 0 with dR /dm < 0 (dR /dm < 0) correspond to asymptotically stable (unstable) distributions. From Fig. 5.34 we read off that there are three qualitatively different parameter regimes. For T /κ > C with C ≈ 0.223 the system is monostable and exhibits the isotropic phase only. For 1/5 < T /κ < C the system is bistable and exhibits a stable isotropic phase, an unstable nematic phase and a stable nematic phase. For T /κ < 1/5 the system is monostable and exhibits a stable nematic phase and an unstable isotropic phase. Finally, Fig. 5.35 shows the bifurcation diagram of the order parameter q. As indicated in Fig. 5.35 for κ/T ∈ [1/C, 5] with 1/C ≈ 4.488 both the isotropic phase with q = 0 and the nematic phase with q > 0 are stable solutions of the mean field model. Note that the loop in Fig. 5.35 describes a hysteresis loop (see also [139]). Let us illustrate the stability of stationary solutions by means of the free energy measure F given by (5.330) (see also [90] and [139, Sect. 10.3]). To this end, we consider a one-parametric family of probability densities 1 A(x)c (5.341) Pc (x) = exp κ Z T with Z = Ω exp{κA(x)c/T } dx and substitute Pc (x) into (5.330). Thus, we obtain F (c) = F [Pc ] with

22 κc κ1 A(x) dx . F (c) = − APc (x) + κc APc (x) − T ln exp 2 T Ω (5.342)

0.08 0.06 F(c) 0.04 0.02 0

0.2

0.6

c

1

Fig. 5.36. Free energy F (c) computed from (5.342). We have plotted the four cases shown in Fig. 5.34. From top to bottom: T /κ = 0.3 (isotropic phase; unique minimum at c = 0), T /κ ≈ 0.223 (saddle node bifurcation point; emergence of the nematic phase), T /κ = 0.21 (bistable regime, two minima at c = 0 and c > 0), and T /κ = 1/5(= 0.2) (the isotropic phase becomes unstable, unique minima at c > 0). Note that the free energies are shifted such that we have F (c = 0) = 0

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1.2 1 0.8 f(c) 0.6 0.4 0.2 0 –0.2

0.1

0.2

0.3

0.4

c

0.5

–0.4

Fig. 5.37. A detail of Fig. 5.36 in order to illustrate the bistable regime; f (c) corresponds to 103 × F (c). We see that at the saddle node bifurcation point (second graph from above) a second minimum occurs. For T /κ = 0.21 (third graph from above) there is a minimum at c = 0 in addition to the minimum at c > 0 shown in Fig. 5.36. For T /κ = 1/5 (bottom graph) the minimum at F (c) vanishes and becomes a maximum

Note that (5.341) and (5.342) are the counterparts to (5.255) and (5.256) discussed in the context of the KSS model. Figures 5.36 and 5.37 illustrate that with respect to the family of distributions Pc the free energy behaves as predicted by the analysis of the self-consistency equation. For T /κ > C the free energy F (c) has a unique minimum at c = 0 indicating that the system is monostable and exhibits the isotropic phase only. For 1/5 < T /κ < C the measure F (c) has a minimum at c = 0 and a minimum at c > 0 related to an isotropic phase and a nematic phase. For T /κ < 1/5 the free energy F (c) has a unique minimum at c > 0, which indicates that the system is monostable and exhibits only one stable phase, namely, the nematic phase. Rotational Diffusion Models Above, we have first derived a free energy measure for the director component nz and, subsequently, we have written a free energy Fokker–Planck equation. More sophisticated models describing liquid crystals in terms of nonlinear Fokker–Planck equations can be obtained by approaching the problem in the opposite way. According to studies by Doi and Edwards [139] and Hess [289], the starting point is a multivariate nonlinear Fokker–Planck equation with a diffusion term that accounts for rotational diffusion. Subsequently, one may reduce the evolution equation to a univariate nonlinear Fokker–Planck equation by exploiting the assumed cylindrical symmetry of the director field [155, 157, 158, 304, 303, 378, 458, 618]. In line with this second approach, we may modify (5.332) and supplement it with a state-dependent mobility coefficient M (x) > 0 (see e.g. [156]).

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5.5.4 Muscular Contraction In line with a proposal by Shimizu and Yamada [528, 529], we will consider next a hydrodynamic muscle model and derive a phenomenological equation for muscular contraction from this model. Figure 5.38 depicts a muscle attached at the bones of two limbs. Before contraction, the muscle has a particular rest length. During contraction the muscle shortens and the relative position of the limbs change. As shown in Fig. 5.38, muscles consist of thin

000 111

bone 000 111 muscle 000 111 000 111 A

000 111 bone 000 111 muscle 000 A 111 000 111 000 111 000 111 000 111

B

B

111 000 000 111 000 111

B

joint

1111111 0000000 0000000 1111111 0000000 1111111

A B

before contraction

00 11 00 11 00 11 00 11 00 11 000000 111111 000000 111111 000000 111111

force: f

joint

000000 111111 111111 000000 000000 111111

A

during contraction

cross bridge

00 11 00 11 00 11 00 11 111111 000000 00 11 000000 111111 000000 111111

b * ( f0 − f ) = ( a + f ) * v Hill’s equation

contraction velocity: v

Fig. 5.38. Simple model of a muscle (upper panel) and Hill’s equation (lower panel) describing the force-velocity relationship during muscular contraction

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and thick filaments [595]. According to the sliding-filament theory, during contraction the thin filaments are pulled closer together, which leads to a shortening of the muscle. The pulling force is established by cross-bridges. Cross-bridges have an active and a passive state. In the active state, crossbridges connect thin and thick filaments and pull the thin filaments closer together by exerting power strokes. In the passive state, they do not connect the filaments but prepare themselves for another power stroke. As a result of this basic mechanism, muscles shorten with particular contraction velocities. The contraction velocity v depends primarily on the force f that is produced during the contraction. Hill’s equation (see Fig. 5.38) is a phenomenological description of the force-velocity relationship. There are two points of the force-velocity curve that have a simple interpretation. First, if a muscle produces its maximum force, it does not shorten at all (i.e., we are dealing with an isometric contraction). Consequently, for f = fmax we have v = 0. Second, if muscles are unloaded, that is, if they do not need to produce a force, then they can contract as fast as possible. In this case, we have f = 0 and v = vmax . In between these two extremes the velocity v monotonically decreases as a function of f . In order to derive Hill’s equation from the sliding-filament theory, Shimizu and Yamada [528, 529] exploited an analogy between sliding filaments and fluids, see Fig. 5.39. Following Shimizu and Yamada, we consider N0 particles that are dispersed in a fluid. Let v and ui denote the velocity of the fluid and the velocities of the particles. If the velocities of the particles differ significantly from the velocity of the fluid, then there is an interaction between the fluid and the particles (hydrodynamic interaction [458]).

N0 particles in solvent v

u1

u3 u2

velocities: v, u1, u2, u3, ...

N0 cross bridges on thin filaments v u1 u2 u3 velocities: v, u1, u2, u3, ...

u = v hydrodynamic interaction u=v no interaction

Fig. 5.39. Scheme of a hydrodynamic muscle model

In a muscle the thin filaments may play the role of the fluid and the cross-bridges may be regarded as the counterparts of the particles. Just as

204


in the case of hydrodynamic interaction, we assume that there is an interaction between the cross-bridges and the thin filaments. It is reasonable to assume that active cross-bridges (i.e., those attached to the thin filaments) are accelerated if their velocities fall behind the filament velocity (which is the contraction velocity) and are de-accelerated if they move faster than the filaments move and the muscle shortens. Likewise, we can assume that the contraction velocity v increases (decreases) if the cross-bridges move on the average faster (slower) than v. Finally, according to the hydrodynamic muscle model, the percentage r ∈ [0, 1] of active muscles depends on the contraction velocity v. These basic relations are summarized in Table 5.4. Table 5.4. Basic relations of the hydrodynamic muscle model Variable

Change

Parameters

ui (t)

ui ⇑ if ui < v ui ⇓ if ui > v v ⇑ if v < mean of ui v ⇓ if v > mean of ui r ⇑ with k+ r ⇓ with k− (v) = c1 + c2 v

u0

v(t) r(t) r(t)

f k+ k− (v)

In detail, the evolution equations for ui , v and r are given by 1 2 d ui (t) = χi (t) λ(u0 − ui ) − γui − κ(ui − v) + QΓi (t) , (5.343) dt N0 d (5.344) χi (t)[ui − v] − f , M v(t) = dt i=1 d r(t) = k + (1 − r) − (b1 + b2 v)r = k + − k − (v)r dt

(5.345)

with λ, γ, κ, k + , b1 , b2 , M > 0 and i = 1, . . . , N0 . Here, we put χk = 1 if the cross-bridge k is active. Otherwise, we have χk = 0. Since we are not interested in the information, which cross-bridge can be found in an active state at a particular time t, we confine ourselves to studying only the behavior of the active cross-bridges. Then, (5.343-5.345) become d ui (t) = −λ(ui − u0 ) − γui − κ(ui − v) + QΓi (t) , dt N0 d M v(t) = r (ui − v) − f , dt i=1

(5.346) (5.347)

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d r(t) = k + (1 − r) − (b1 + b2 v)r . (5.348) dt Let us first evaluate the deterministic case: Q = 0. In thiscase, the stationary states are given by ui,st = (λu0 + κvst )/(λ + γ + κ), rst i (ui,st − vst ) = f , and rst = k + /(k + + b1 + b2 vst ), which gives us b [f0 − f ] = (a + f )vst , k − (v)

(5.349)

with b = (k + + b1 )/b2 , f0 = k + N0 λu0 /[(k + + b1 )(λ + γ + κ)] and a = k + N0 (λ + γ)/[b2 (λ + γ + κ)]. Consequently, from the hydrodynamic muscle model we can derive Hill’s empirical equation. As indicated in (5.349) the mixed term f vst results from the assumption that the decrease of the number of active cross-bridges depends on the contraction velocity. In order to study time-dependent solutions of (5.346-5.348), we put again Q = 0 and assume that v(t) and r(t) evolve much faster than ui (t). Using adiabatic elimination [254, 255], we obtain r(t)[ i (ui (t)−N0 v(t)] = f N0 and r(t) = k + /[k + + b1 + b2 v(t)], where f = f /N0 denotes the contraction force per available cross-bridge. Consequently, we can eliminate r(t), express v(t) in terms of v(t) = [k + N0−1 i ui (t) − f (k + + b1 ]/[f b2 + k + ], and transform (5.346) into N0 d 1 ui (t) = −λeff (ui − ui,st ) − κeff ui − (5.350) uk , dt N0 k=1

with λeff = λ + γ + κ[1 − k √ /(k + b2 f )] > 0 and κeff = κ k + /(k + + b2 f ). Taking the fluctuating force QΓi into account, for Xi = ui − ui,st we obtain the multivariate Langevin equation N0 1 d Xk + QΓi (5.351) Xi (t) = −λeff Xi − κeff Xi − dt N0 +

+

k=1

that in turn reduces to d X(t) = −λeff X − κeff (X − X) + QΓ , (5.352) dt if we use the limit N0 → ∞, assume that Xk are statistically-independent random variables at an initial time t0 , and assume that Xk are distributed the same way at time t0 (see Sect. 3.8). That is, the hydrodynamic muscle model can be evaluated by means of the Shimizu–Yamada model described in Sect. 5.2.1. Since we have λeff > 0, we obtain in any case a stationary Gaussian distribution for the cross-bridge velocities ui . In closing these considerations, we would like to point out that in order to derive (5.352) we have applied adiabatic elimination to the deterministic evolution equation. The method of adiabatic elimination, however, can also be applied to stochastic evolution equations [197, 254, 511].

206


5.5.5 Network Models for Group Behavior We briefly address here two network models that can describe the emergence of group behavior in populations of humans and animals and that are used in Sects. 5.2.2 and 7.3.2 to illustrate the basins of attraction of stationary distributions and the emergence of reentrant phase transitions. Network Interpretation of the Dynamical Takatsuji Model We discuss first the network model shown in Fig. 5.40 related to the dynamical Takatsuji model discussed in Sect. 5.2.2. Let Xi ∈ Ω = lR describe the behavior of the ith member of a population with N0 members. Let us assume that Xi = 0 describes the stationary behavior of an isolated subject of the population and that the relaxation to this stationary behavior in the √ presence of a fluctuating force can be described by dXi /dt = −a1 Xi + QΓi (t) with a1 > 0. Let us further assume that the member i receives input from all other fellow-members at particular interfaces depicted in Fig. 5.40 as circles. In the context of the dynamical Takatsuji model, we consider a lin-

Xk Xk Xi

Fig. 5.40. Interpretation of the dynamical Takatsuji model in terms of a network model for interacting population members

ear conversion of the inputs Xk at the interfaces such that we obtain the converted inputs Xk = a3 Xk with a3 > 0. The converted inputs Xk are averaged and the result is coupled to the internal dynamics using a nonlinear conversion function √ S(z). Therefore, the stochastic differential equation dXi /dt = −a1 Xi + QΓi (t) becomes N0 d 1 Xi (t) = −a1 Xi + S Xk + QΓi (t) , (5.353) dt N0 k=1

5.5 Applications

207

with i = 1, . . . , N0 . A typical nonlinear conversion function S(z) that involves a saturation domain (i.e., we have S(z → ±∞) = ±Ssat ) is given by S(z) = a2 tanh(z) with a2 > 0. Using this choice together with Xk = a3 Xk , we obtain the network model N0 d a3 Xk + QΓi (t) . (5.354) Xi (t) = −a1 Xi + a2 tanh dt N0 k=1

As show in Sect. 3.8, in the limiting case N0 → ∞ we may equate the ensemble of members {X1 , . . . , XN0 } with the statistical ensemble {X 1 , . . . , X N } of an arbitrary member and study the many-body system described by (5.354) in terms of the self-consistent Langevin equation d X(t) = −a1 X(t) + a2 tanh[a3 X(t)] + QΓ (t) . dt

(5.355)

This Langevin equation corresponds to √ the dynamical Takatsuji model (5.163) for a1 = γ + c and a2 = a3 = c (see also (5.179)). As discussed in Sect. 5.2.2 the dynamical Takatsuji model can describe a phase transition between a phase of indecisive members (e.g. undecided voters) with N0 q = N0−1 k=1 Xk = 0 and a phase of determined members (e.g. decided voters) with q = 0. The latter phase occurs with two types: q > 0 and q < 0. Network Model for Reentrant Phase Transitions of Group Behavior The previous network model exhibits a linear conversion at the interfaces between population members and a nonlinear conversion of the overall input. Let us discuss now the opposite situation as shown in Fig. 5.41. According to

Xk Xk Xi

Fig. 5.41. A network model for reentrant phase transitions that occur in populations with interacting members

208


Fig. 5.41, we assume that the behavior of an isolated subject is determined by the stochastic evolution equation dXi /dt = f (Xi , Γi ), where Γi (t) denotes a Langevin forces. We assume that the dynamics involves multiplicative noise: f (X, Γ ) = h(x) + g(x; Q)Γ , where Q denotes the overall amplitude of the noise. Such multiplicative noise typically reflects the impact of a fluctuating pumping force (e.g., a supply with food or information that involves some kind of erraticness) [298]. We assume a nonlinear conversion of the inputs from other population members such that the converted inputs Xk are given by Xk = S(Xk ) (see circles in Fig. 5.41). We further assume that the converted inputs are averaged and that the result couples linearly to the internal dynamics. Thus, we obtain N0 d κ Xi (t) = h(Xi ) + Xk + g(Xi ; Q)Γi (t) , N0 dt

(5.356)

k=1

with i = 1, . . . , N0 . Apart from the tanh-function, we may use the arctanfunction as a nonlinear function that involves a saturation domain. √ conversion √ For S(z) = arctan( bz)/ b we obtain N0 √ d κ arctan( bXk ) + g(Xi ; Q)Γi (t) . Xi (t) = h(Xi ) + √ dt bN0 k=1

(5.357)

Using mean field theory, in the limit N0 → ∞ we may study the network model defined by (5.357) in terms of a single subject described by X(t), where the behavior X(t) is determined by the Langevin equation E √ d κ D X(t) = h(X) + √ arctan( bX) + g(X; Q)Γ (t) dt b

(5.358)

and the corresponding nonlinear Fokker-Planck equation. In Sect. 7.3.2 we will study the properties of this network model in detail. In order to analyze the network model conveniently, we will make however two minor modifications. First, we will replace h(x) by h(x) − κS(x). Second, we will use a slightly modified arctan-function that exhibits however the same basic properties as the arctan-function. Both modifications are not considered as key issues of the network model. The replacement h(x) → h(x) − κS(x) might be interpreted as a feedback of the output Xi to the input interfaces N0 such N0 [Xk − Xi ] instead of κN0−1 k=1 Xk . that in (5.356) we have κN0−1 k=1 Taking these two modifications into account, as we will see in Sect. 7.3.2 the network model (5.357) describes two subsequent phase transitions. The first transition N0 is a phase transition from a phase of indecisive members with q = N0−1 k=1 Xk = 0 to a phase of determined members with q = 0, when the noise amplitude Q becomes larger than a critical value Q1 . That is, the noise results in a process of collective decision making or in the emergence of a collective behavior.The second transition is a phase transition from the

5.5 Applications

209

phase of determined members with q = 0 back to the phase of indecisive members with q = 0 and occurs when Q becomes larger than a critical value Q2 (with Q2 > Q1 ). That is, too much noise destroys the previously obtained collective decision or behavior. 5.5.6 Multistable Perception-Action Systems Perception-action systems of humans and animals that exhibit multiple stable coordination patterns under the same circumstances are said to be multistable. This kind of multistability has been found in animal locomotion [299, 427], rhythmic single limb movements (see below), and rhythmic multilimb movements [15, 16, 51, 264, 334, 412, 461, 476, 487]. Multistability has also been observed in discrete movements such as hitting a ball with a table tennis bat [544] and in coordinated oscillatory movements that involve more than one limb and more than one oscillation frequency (e.g., polyrhythmic drumming movements) [110, 133, 265, 472, 473, 474, 475, 549]. Multistable perception-action systems can be described by dynamical systems involving potential functions with multiple minima. Each minimum of such a potential function (or potential) corresponds to a stable coordination pattern. This is illustrated in Fig. 5.42 for a bistable system. Accordingly, the double-well potential V (x) can be regarded as an energy measure or a measure of effort, where x represents a suitably chosen state variable. Stable perception-action systems occupy states of minimal effort or energy, that is, they occupy a minimum of the potential V [49, 259, 335, 594]. If a perception-action system is initially located outside a potential minimum, then it performs an overdamped energy-decreasing motion and finally converges to a minimum. Consequently, in the deterministic case, we find a bistable perception-action system in either one of the two minima depicted in Fig. 5.42. In order to take fluctuations into account, we may follow the conventional approach and regard the multistable perception-action system as a zero-dimensional unit. In this case, we describe the system in terms of a linear Fokker–Planck equation with additive noise involving the potential V (x) [108, 111, 197, 214, 461, 512]. The stationary state of the perception-action system is then described by a Boltzmann distribution of V (x), see Fig. 5.42. This approach predicts a unique solution and, therefore, fails to account for the phenomenon of multistability. Therefore, we may regard multistable perception-action systems as spatially extended many-body systems composed of interacting components (e.g., neural oscillators) [189]. In this case, we can describe multistable perception-action systems by means of nonlinear Fokker–Planck equations involving potentials V (x) and stochastic feedback in terms of mean field forces arising from the interactions among the components. Such models may exhibit for the same control parameters multiple stationary probability densities as depicted in Fig. 5.42 and as demonstrated in detail, for example, for the Desai–Zwanzig model. Consequently, spatially extended models exhibiting

210


stochastic feedback can describe multistable perception-action system in the presence of noise.

V(x)

V(x)

a)

x

x V(x) b) P(x) x V(x)

V(x) P(x)

c) P(x) x

x

Fig. 5.42. Examples of dynamical models involving a double-well potential V (x): a) deterministic model, b) stochastic zero-dimensional model, c) stochastic spatially extended model. The black balls describe the stationary states of the model a); P (x) corresponds to the stationary probability densities of the models b) and c) [189]

Paced Rhythmic Single Limb Movements Let us briefly discuss an example of a multistable action-perception system. In a seminal work, Kelso and his colleagues have proposed to study paced rhythmic finger movements from the perspective of dynamical systems theory [335, 337]. This multistable perception-action system is of particular importance for human movement sciences because, on the one hand, it shows a variety of interesting phenomena and, on the other hand, it is easily accessible for experimental observation and manipulation. In several experiments subjects were asked to move single limbs such as an index finger or a forearm in a rhythmic fashion along with the beat of a metronome or an oscillating visual pacing signal [51, 109, 110, 337, 335, 338, 259, 631]. They were requested to move on the beat (on-beat condition) or off the beat (off-beat condition).

5.5 Applications

211

In this context, off the beat means that they tapped between two consecutive beats of the metronome or moved into the opposite direction of the visual pacing signal. During the experiments the frequency of the beats was gradually increased. At low pacing frequencies both off-beat and on-beat movements could be stably performed, whereas at high pacing frequencies only the onbeat condition could be performed in a stable fashion. If the subjects were asked to move off-beat, then often involuntary switches occurred from the required off-beat pattern to the on-beat pattern when the pacing frequency exceeded critical (subject-dependent) values. This involuntary transition from the off-beat to the on-beat coordination pattern has been interpreted as a nonequilibrium phase transition [49, 215, 216, 262, 312, 313, 314, 315, 335]. From this observation, it has been concluded that paced rhythmic limb movements involve a perception-action system that is bistable in a particular parameter regime and monostable in another. In order to account for the multistability of paced limb movements and to model the transitions between different patterns of paced limb movements, nonlinear Fokker–Planck equations have been used in a series of studies [171, 173, 198, 199, 201]. In these studies it was assumed that the primary part of the perception-action systems involved in the performance of paced limb movements can be modeled in terms of phase oscillator populations, see Sect. 5.5.2. These phase oscillator ensembles, in turn, have been described by means of the mean field HKB model discussed in Sect. 5.3.3. In the context of the mean field HKB model, the potential force h(x) = −dVHKB (x)/dx describes a driving force that results from the pacing signal and acts on each oscillator phase Xk , whereas the sine coupling-force describes the couplings between the neural oscillators. The phase transitions described by the mean field HKB model and illustrated in Figs. 5.28d and 5.29d are assumed to reflect the phase transitions observed in the experiments.

6 Entropy Fokker–Planck Equations

In Sect. 2.6 free energy Fokker–Planck equations with linear energy functionals U have been referred to as entropy Fokker–Planck equations. In line with (4.49), we define entropy Fokker–Planck equations by ∂ ∂ ∂ δF P (x, t; u) = M (P )P ∂t ∂x ∂x δP

(6.1)

in the univariate case and ∂ δF P (x, t; u) = −∇ · {IP } + ∇ · M(P )P · ∇ ∂t δP

(6.2)

in the multivariate case, where F is given by F [P ] = UL [P ] − QS[P ]

(6.3)

and UL describes a linear functional. That is, UL is given by UL [P ] = U (x)P (x) dx in the univariate case and UL [P ] = Ω U0 (x)P (x) dM x in Ω 0 the multivariate case. Using entropy and information measures of the form (4.5), entropy Fokker–Planck equations can be written as dU0 (x) ∂ ∂ ∂ δS P (x, t; u) = M (P )P −Q ∂t ∂x dx ∂x δP 6 7 ∂ dU0 (x) dB ∂ ˆ = M (P ) (6.4) P +Q Ls (P ) ∂x dx dz z0 ∂x and ∂ δS P (x, t; u) = −∇ · {[I − M · ∇U0 (x)] P } + Q∇ · MP · ∇ ∂t δP dB ˆ s (P ) , = −∇ · {[I − M · ∇U0 (x)] P } + Q ∇ · M · ∇L dz z0 (6.5) with z0 given by z0 =

Ω

ˆ s defined by (4.6) [190, 191]. s(P ) dM x and L

214


Canonical-Dissipative Systems Nonlinear Fokker–Planck equations of canonical-dissipative systems of type B defined by (4.101) can be regarded as entropy Fokker–Planck equations because they involve linear internal energy functionals (see (4.99)). Stationary Solutions We confine ourselves to considering entropy Fokker–Planck equations for which the drift and diffusion coefficients and the boundary conditions are defined such that stationary solutions can be derived from the free energy principle (4.17). Consequently, in the univariate case, stationary solutions can be obtained by substituting the functional U = UL [P ] = Ω U0 (x) P (x) dx into (4.20), which leads to ⎞ ⎛ −1 ds ⎜ U0 (x) − µ ⎟ (6.6) Pst (x) = ⎠ , ⎝ dB(z0,st ) dz Q dz with z0,st = Ω s(Pst ) dx. In the multivariate case, from (4.20) stationary solutions of the entropy Fokker–Planck equation (6.5) can be found as ⎞ ⎛ −1 ds ⎜ U0 (x) − µ ⎟ (6.7) Pst (x) = ⎠ , ⎝ dB(z0,st ) dz Q dz with z0,st = Ω s(Pst ) dM x. Approach to Stationary Solutions If S is concave, then the free energy measure (6.3) is bounded from below (see case A in Table 4.2). Consequently, the H-theorem of free energy Fokker– Planck equations (see Sect. 4.3) can be used to prove that transient solutions of entropy Fokker–Planck equations converge to stationary ones in the long time limit: ∂ P =0. (6.8) lim t→∞ ∂t Stability of Stationary Solutions As stated in Sect. 4.1, stationary distributions derived from the free energy principle (4.17) correspond to critical points of the free energy F . That is, the first variation of F vanishes with respect to the space of probability densities. In symbols: we have δF [Pst ]() = 0 for perturbations that yield probability

6.1 Existence and Uniqueness of Stationary Solutions∗

215

densities again. Due to the linearity of UL the second variation of F is given by δ 2 F = −Qδ 2 S . (6.9) In general, for concave entropy and information measures and linear internal energy functionals, stationary distributions defined by the free energy principle correspond to free energy minima, see (4.133). In particular, for entropy and information measures that can be cast into the form S = B( Ω s(P ) dM x) and satisfy the conditions listed in (6.81), it follows that the inequalities δ 2 S[P ] < 0 in general and δ 2 S[Pst ] < 0 in particular hold (see Sect. 6.4.1), which implies that we have δ 2 F [P ] > 0 in general and δ 2 F [Pst ] > 0 in particular. That is, we are dealing again with stationary distributions that correspond to free energy minima. If we replace (5.20) by means of (6.9), then linear stability analysis and stability analysis by means of Lyapunov’s direct method can be carried out as discussed in Sect. 5.1 and one finds that the stationary solutions (6.6) are asymptotically stable because they correspond to free energy minima. δ 2 S as a Lyapunov Functional For entropy and information measures with δ 2 S[Pst ] < 0 the norm (5.27) reads (6.10) = δ 2 F [Pst ]() = −Q δ 2 S[Pst ]() . As argued above, a linear stability analysis similar to the one discussed in Sect. 5.1 can be carried out and thus the inequality d /dt < 0 for = 0 and the limiting case = 0 for t → 0 can be obtained (see (5.28)). From the inequality d /dt < 0 it follows that perturbations (x, t) of stationary solutions of entropy Fokker–Planck equations satisfy d 2 δ S[Pst ]() > 0 . dt

(6.11)

In particular, for S given by (6.81) we have δ 2 S < 0 for = 0 and δ 2 S = 0 ⇔ = 0 (see (6.82) and (6.83)), which gives us δ 2 S → 0 in the limit t → ∞. In this case δ 2 S corresponds to a Lyapunov functional. Note that this interpretation of δ 2 S has also been given in nonequilibrium thermodynamics for the special case in which S corresponds to the Boltzmann entropy [228, 353, 449].

6.1 Existence and Uniqueness of Stationary Solutions∗ As was demonstrated in Sect. 4.7.1, stationary solutions of free energy Fokker–Planck equations can be expressed by means of Boltzmann distributions and distortion functionals. In what follows, we will use distortion functionals in order to show that stationary solutions of entropy Fokker–Planck

216


equations exist and are unique [192]. To this end, we consider measures S given by

s(P ) dM x , S[P ] = Ω

ds →∞, lim z↓0 dz

(6.12)

and d2 s/ds2 < 0. The latter condition implies the concavity of the functional S (see Sect. 6.4.1). Substituting (6.12) and UNL = 0 into (4.112), we obtain the relations ds dG G(z) = exp − − 1 , lim G(z) = 0, >0. (6.13) z↓0 dz dz From these relations, we see that the mapping G(z) is invertible. We distinguish between two cases: G(z) is bounded from above and G(z) is not bounded from above. For the sake of convenience, we formally define the maximum value of G by Gc : limz→∞ G(z) = Gc < ∞ . (6.14) Gmax = ∞ : limz→∞ G(z) → ∞ Consequently, if Ω −1 denotes the domain of definition of G−1 , we have Ω −1 = (0, Gmax ). From (4.116) it follows that 1 W (x) (6.15) Pst (x) = G−1 Z holds. That is, Pst can be computed from the Boltzmann distribution W (x) = exp{−U0 (x)/Q}/ZB with ZB = Ω exp{−U0 (x)/Q} dM x by means of a mapping that distorts the shape of W . Note that in (6.15) the constant Z is confined to the interval Z > Wmax /Gmax , where Wmax denotes the maximum of W (x). The next objective is to determine Z. From (6.13) and (6.14) it follows that G−1 (z ↓ 0) = 0,

dG−1 > 0, dz

lim

z→Gmax

G−1 (z) → ∞ .

We define the normalization integral

1 −1 W (x) dM x n(Z) = G Z Ω

(6.16)

(6.17)

on Z ∈ (Wmax /Gmax , ∞). Due to the relations given in (6.16), the integral n(z) satisfies

6.1 Existence and Uniqueness of Stationary Solutions∗

lim n(Z) = 0 ,

217

(6.18)

Z→∞

1 dn(Z) dG−1 =− 2 W (x) dM x < 0 . Z Ω dz z=Z −1 W (x) dZ

(6.19)

>0

Consequently, n(Z) is a strictly monotonically decreasing function that vanishes in the limit Z → ∞. The question arises whether or not there is a Z such that n(Z) is larger than or equal to unity. To answer this question, we treat the cases Gmax = ∞ and Gmax = Gc separately. For Gmax = ∞ we consider a subset ω ⊂ Ω for which W (x) is larger than or equal to a constant C (i.e., ∀x ∈ ω : W (x) ≥ C). Then, one obtains the inequality

C C dM x = G−1 dM x . (6.20) G−1 n(Z) ≥ Z Z ω ω >0

Since Gmax = ∞ the integral n(Z) is defined on Z ∈ (0, ∞) and we can consider the limiting case Z → 0. It is clear that in this case we obtain

C →∞. (6.21) dM x lim G−1 lim nS (Z) ≥ Z↓0 Z↓0 Z ω In sum, for Gmax = ∞ the integral n(Z) is not bounded from above. In the case Gmax = Gc we exploit the fact that n(Z) is a monotonically decreasing function. Therefore, the maximum value of n(Z) is given for the smallest possible value of Z, which is Z = Wmax /Gmax : Wmax . (6.22) max {n(Z)} = n Z ↓ Gc Z∈(Wmax /Gc ,∞) Equations (6.21) and (6.22) can be summarized as follows:

limZ↓Wmax /Gc Ω G−1 Z1 W (x) dM x : limz→∞ G(z) = Gc < ∞ . nmax = ∞ : limz→∞ G(z) → ∞ (6.23) If this maximum value equals one or is larger than one, then there is a unique Z ∗ ∈ (Wmax /Gmax , ∞) that yields n(Z ∗ ) = 1 and we can write (6.15) as 1 −1 W (x) . (6.24) Pst (x) = G n−1 (1) In sum, for distortion functionals G without an upper boundary the existence of Z ∗ = n−1 (1) is guaranteed. In contrast, if G is bounded from above by Gc , we need to make an additional effort to verify that Pst can be written in the form of (6.24): we need to check if there is at least one Z > Wmax /Gmax that gives us a value n(Z ) ≥ 1 (which means that we do not necessarily need to determine nmax ).

218


6.2 Entropy Increase and Anomalous Diffusion For UL = 0 the entropy Fokker–Planck equation (6.1) becomes ∂ ∂ ∂ δS P (x, t; u) = −Q M (P )P , ∂t ∂x ∂x δP

(6.25)

which can be expressed as ∂ ˆ dB ∂ ∂ M (P ) L P (x, t; u) = Q s (P ) , ∂x ∂t dz z0 ∂x

(6.26)

for S[P ] given by (4.5). In the linear case (i.e., for S = BS = − P ln P dx and M (P ) = 1) the diffusion term is linear with respect to P and we obtain the Fokker–Planck equation of univariate Wiener processes, ∂ ∂2 P (x, t; u) = Q 2 P , ∂t ∂x

(6.27)

see Sect. 3.9.4. Let us study two fundamental properties of the solutions of (6.25). 6.2.1 Entropy Increase It appeals to our intuition that diffusion processes result in an increase of the disorder of the systems in which they take place. The increase of disorder may be measured in terms of an increase of the entropy of the systems or an increase of the information that is necessary to describe the systems. Indeed, the Boltzmann entropy BS increases for solutions of the linear diffusion equation (6.27). From (6.27) we obtain by means of partial integration d B S[P ] = Q dt

Ω

1 P

∂ P ∂x

2 dx ≥ 0 .

(6.28)

In order to derive (6.28) we have assumed that the surface term that arises due to the integration by parts vanishes. From (6.28) it is clear that BS is a monotonically increasing function with respect to t. For the more general case given by (6.25) a similar result holds [163]. In order to verify this, we differentiate S with respect to t, eliminate ∂P/∂t by means of (6.25), integrate by parts and assume that the surface term thus obtained vanishes. Then, we obtain 2

d ∂ δS P dx ≥ 0 . (6.29) S[P ] = Q dt ∂x δP Ω That is, in line with linear nonequilibrium thermodynamics, the entropy production di S = dS is semi-positive (see also Sect. 4.5.1).

6.2 Entropy Increase and Anomalous Diffusion

219

6.2.2 Anomalous Diffusion We consider now stochastic processes subjected to natural boundary conditions and put Ω = lR. As we have shown in Sect. 3.9.4, the variance K of solutions of the linear diffusion equation (6.27) increases linearly with t: K(t) ∝ t. Diffusion that exhibits such a linear relationship is referred to as normal diffusion. If the graph K(t) differs from a linear function, we deal with anomalous diffusion (see Sect. 1.4.5). In recognition of this classification, the question arises as to what kind of diffusion processes (normal or anomalous diffusion) are described by nonlinear diffusion equations of the form (6.25). Our aim now is to answer this question without knowing the explicit form of the measure S that occurs in (6.25). We will show that the crucial issue is not the explicit form of S but the extensivity or nonextensivity of S. Composability, Extensivity, and Nonextensivity Following [170], we will examine this relationship for entropy and information measures that satisfy S[P P ] = S[P ] + S[P ] + G(S[P ], S[P ]) .

(6.30)

Here, P and P are distributions defined on Ω and Ω and the product P P is regarded as a distribution P defined on Ω × Ω . Equation (6.30) says that if we combine two statistically-independent systems described by P and P and the joint distribution P = P P , then the entropy and information of the combined system can be computed from the entropy and information measures of the single systems. We say that measures S that satisfy (6.30) are composable (see also Sect. 6.4.1). The function G(u, v) denotes an arbitrary function of the subsystem entropies S[P ] and S[P ]. Note that the commutativity of the multiplication (i.e., P P = P P ) implies the symmetry of G (i.e., we have G(u, v) = G(v, u)). If G depends on u (or v), then S corresponds to a nonextensive measure, see Sect. 6.4.1. In contrast, for G = const., we can introduce the shifted functional S = S + G, which satisfies the relation of extensive entropies [261, 625]: S [P P ] = S [P ] + S [P ] .

(6.31)

Therefore, for G = constant and in particular for G = 0 we consider S as an extensive measure. Evolution Equation for K From (6.26) we can derive the evolution equation of the first and second moments:

220


d X = 0 , dt

d 2 dB ˆ s dx . X = 2Q L dt dz z0 Ω

(6.32) (6.33)

ˆ s into (6.33), for K(t) = X 2 − X2 Substituting the definition (4.6) of L we then find 7 6 ds(z) d dB s(P (x, t; u)) − P (x, t; u) dx . K(t) = 2Q dt dz z0 Ω dz z=P (x,t;u) Y [P ] (6.34) Consequently, if the functional Y [P ] is constant with respect to time we have normal diffusion (i.e., K(t) ∝ t). Otherwise, we find anomalous diffusion (i.e., K(t) ∝ t). We now derive Y from the assumed nonextensivity/extensivity property (6.30). To this end, let P (x) be defined on the real line and P (y) be defined on the interval [0, a] with a > 0. Furthermore, let P (y) denote the uniform distribution on [0, a], that is, P (y) = 1/a. Then, from (6.30) and S = B[ Ω s(P ) dx] it follows that 1 1 P (x) dx = S[P ] + B as + G S[P ], B as . s B a a a a Ω (6.35) Next, we differentiate (6.35) with respect to a and put a = 1. Thus, we obtain ∂G(S[R1 ], v) Y [R1 ] = C + , (6.36) ∂v v=C

with C=

s(1)−

ds(z) dB(z) . dz z=1 dz z=s(1)

Consequently, the variance K(t) satisfies the evolution equation d ∂G(S[P ], v) K(t) = 2QC + 2Q , dt ∂v v=C

(6.37)

(6.38)

with P (x, t; u) determined by (6.26). Since C does not depend on the time variable t, we deal with normal diffusion if the second term on the righthand side of (6.38) does not depend on time. Otherwise, we find anomalous diffusion. Therefore, at issue is how S[P ] and ∂G(S[P ], v)/ ∂v|v=C evolve as functions of time. From (6.29) it follows that S[P ] satisfies the relation 2 2

∂ ds(z) d dB P (x, t; u) dx ≥ 0 . S[P ] = Q dt dz z0 ∂x dz z=P (x,t;u) Ω (6.39)

6.2 Entropy Increase and Anomalous Diffusion

221

We require now that the entropy functional S is sensitive to unlikely events. More precisely, we require the existence of an interval (0, l] of finite length l (i.e., l > 0) such that the derivative ds(z)/ dz maps all elements of (0, l] to nonvanishing function values (i.e., ∃ l : ∀z ∈ (0, l] : ds(z)/ dz = 0). We find that for entropies of this kind the expression ∂ ds(z) (6.40) ∂x dz z=P (x)

can have at most a finite number of zeros for x ∈ Ik , where the intervals Ik are defined by Ik = [xkl , xkr ] with xkl < xkr , Ik mutually disjoint, and 0 < P (z) ≤ l for all z ∈ Ik . That is, ∂ds/ ∂xdz = 0 for z = P (x) and x ∈ Ik . Since we restrict our considerations to continuous probability densities which decay to zero in a continuous fashion (i.e., we assume P ∈ C(Ω)), the existence of such intervals is guaranteed. From (6.39) we can then read off that 2 2

dB d ∂ ds(z) S[P ] ≥ Q P (x, t; u) dx > 0 . dt dz z0 ∂x dz z=P (x,t;u) Ik k (6.41) In sum, entropies which are sensitive to unlikely events are strictly monotonically increasing functions for solutions of (6.26). We are now in the position to examine the evolution of ∂G(S[P ], v)/ ∂v|v=C . Differentiating this expression with respect to t yields dS[P ] d ∂G(S[P ], v) ∂ 2 G(u, v) = . (6.42) ∂u∂v v=C,u=S[P ] dt dt ∂v v=C Using this result and differentiating (6.38) with respect to t, we obtain dS[P ] ∂ 2 G(u, v) d2 K(t) = 2Q . (6.43) dt2 ∂u∂v v=C,u=S[P ] dt >0 F Therefore, we have normal diffusion (i.e., we have d2 K(t) dt2 = 0) if and only if ∂ 2 G(u, v) =0. (6.44) ∂u∂v v=C,u=S[P ] Since the extensivity and nonextensivity, respectively, can be defined by means of the derivative ∂G(u, v)/ ∂u|u=S[P ] (see above), we can now draw our final conclusions (which are only valid within the framework of nonlinear Fokker–Planck equations and composable entropies, of course). –

Extensive systems show normal diffusion. Nonextensive systems with ∂G(u, v)/ ∂v|v=C = 0 show normal diffusion. Normal diffusion only occurs in nonextensive systems with ∂G(u, v)/ ∂v|v=C = 0 and extensive systems.

222

–


Nonextensive systems with ∂G(u, v)/ ∂v|v=C = 0 show anomalous diffusion. Anomalous diffusion only occurs in nonextensive systems satisfying ∂G(u, v)/ ∂v|v=C = 0.

Roughly speaking, nonextensivity implies anomalous diffusion and extensivity implies normal diffusion. But there is an exception to this rule: in nonextensive systems for which the first order partial derivative of G(u, v) with respect to u vanishes for u = C normal diffusion can also occur. Let us conclude our considerations about the relationship between anomalous diffusion and nonextensivity with two remarks. First, in the absence of an outer function B (i.e., for B(z) = z) we usually find s(1) = 0. The reason for this is that for B(z) = z many entropy functionals S are derived from N entropies S = i=1 s(pi ) for discrete sets of probabilities pi . In these cases, by convention, one often defines s(z) in such a way that it vanishes in the case of a certain event such that S = 0 for pi = 1 and ∀k = i : pk = 0. For B(z) = z and s(1) = 0 the constant C reads C = − ds(z)/ dz|z=1 . In this special case, the evolution of the variance is described by d ds(z) ∂G(S[P ], v) K(t) = −2Q + 2Q . (6.45) dt dz z=1 ∂v v=− ds(z)/dz|z=1 In particular, for the Boltzmann entropy BS = − P ln P dx we obtain ds(z)/ dz = −1−ln z and the relation dK(t)/ dt = 2 Q ⇒ K(t) = 2Q(t − t0 ) derived earlier for univariate Wiener processes. Second, the derivation presented here does not hold for diffusion processes with infinite variances such as Lévy distributions [429, 533]. In this context, several limitations of the approach to anomalous diffusion by means of nonlinear Fokker–Planck equations and the calculation of variances have been uncovered [191, 192]. In order to circumvent such problems, one may follow Tsallis and Bukman who introduced the notion of pseudo anomalous diffusion for Lévy distributions and used time-dependent normalization constants instead of variances to address the issue of anomalous diffusion [591].

6.3 Drift- and Diffusion Forms Univariate Case There are two special cases of (6.4) in which either the drift term or the diffusion term become linear with respect to P [190]. For M (P ) = 1 the nonlinear Fokker–Planck equation (6.4) can be written as dB ∂ 2 ˆ ∂ ∂ (6.46) Ls (P ) , P (x, t; u) = − h(x)P + Q ∂t ∂x dz z0 ∂x2 where h(x) is defined by h(x) = −dU0 (x)/dx. We refer to (6.46) as the diffusion form of the entropy Fokker–Planck equation (6.4) because it is the

6.3 Drift- and Diffusion Forms

223

diffusion term that makes (6.46) nonlinear with respect to P . Now, let us chose M (P ) such that the diffusion term of (6.4) becomes linear. That is, we require that the equivalence dB ∂ ˆ ∂ M (P ) P (6.47) Ls (P ) = ∂x dz z0 ∂x holds. Solving (6.47) for M gives us 6 7−1 ˆ s (P ) dB dL M (P ) = . dz z0 dP ˆ s (P )/dP = −P d2 s(P )/dP 2 holds, we write (6.48) as Since dL −1 dB d2 s(P ) M (P ) = − P dz z0 dP 2

(6.48)

(6.49)

with z0 = Ω s(P ) dx. In particular, for concave entropy and information measures of the form (6.81), the mobility coefficient (6.49) is nonsingular and welldefined because the concavity property leads to dB(z0 )/dz d2 s(P )/dP 2 < 0. For mobility coefficients M (P ) described by (6.48) and (6.49) the entropy Fokker–Planck equation (6.4) can be expressed as ∂ P ∂ ∂2 P (x, t; u) = − h(x) + Q 2 P (6.50) ˆ s (P )/dP ∂t ∂x ∂x dB( Ω s(P ) dx)/dz dL and h(x) ∂ ∂ ∂2 P (x, t; u) = P . + Q ∂t ∂x |dB( Ω s(P ) dx)/dz d2 s(P )/dP 2 | ∂x2

(6.51)

We refer to these equations as drift forms of the entropy Fokker–Planck equation (6.4). Multivariate Case The multivariate case can be treated in a similar vein [193]. For M(x, t, P ) = M(x, t) and I(x, t, P ) = I(x, t) the evolution equation (6.5) reads ∂ P (x, t; u) = −∇ · [I(x, t) − M(x, t) · ∇U0 (x)]P ∂t dB ˆ s (P ) ∇ · M(x, t) · ∇L +Q dz z0

(6.52)

and corresponds to the diffusion form of the entropy Fokker–Planck equation (6.5). In contrast, if we use for M an expression similar to (6.48), namely,

224


⎡

dB ⎣ M(x, t, P ) = dz

M

Ω

s(P ) d

x

⎤−1 ˆ s (P ) dL ⎦ M (x, t) , dP

(6.53)

then (6.5) becomes ∂ P (x, t; u) = −∇ · ∂t

with z0 =

6

M (x, t) · ∇U0 (x) I(x, t, P ) − ˆ s (P )/dP dB(z0 )/dz dL

7

+Q∇ · M (x, t) · ∇P ,

Ω

P (6.54)

s(P ) dM x. Equation (6.54) is the drift form of (6.5).

6.4 Entropy and Information Measures In this section, we will consider entropy functionals and information measures S = S[P ]

(6.55)

that describe mappings from continuous probability densities P to the set of real numbers. We will discuss some elementary properties that are usually satisfied by measures of this kind. 6.4.1 Properties∗ Continuous and Differentiable Let us define a measure S that acts on continuous probability densities P by

S[P ] = B s[P (x)] dM x , Ω

s(z) ∈ C ([0, ∞)), s(z) ∈ C ∞ ((0, ∞)) , B(z) ∈ C ∞ (Ωcod ) . 0

(6.56)

The function B(z) is defined on the range of values of the functional s[P (x)] dM x (i.e., the co-domain) denoted by Ωcod :

Ωcod = {y| y = s[P (x)] dM x , P (x) ∈ C 0 (Ω), P > 0} . (6.57) Ω

The kernel s(z) is continuous on z ∈ [0, ∞) and infinitely differentiable for z > 0. Furthermore, we require that the scale function B is infinitely differentiable on Ωcod . On account of these properties, we assume that the variations δS and δ 2 S and the functional derivatives δS/δP , and δ 2 S/δP 2 exist for positivedefinite probability densities (i.e., for P with P > 0). The first and second variations of S are defined by means of the Taylor expansion

6.4 Entropy and Information Measures

1 S(P + ) = S(P ) + δS[P ]() + δ 2 S[P ](2 ) + O(3 ) , 2

225

(6.58)

which gives us δS[P ]() =

dB(z) dz

M

Ω

s(P ) d

x

Ω

ds(z) (x) dM x dz P (x)

(6.59)

and 2

d2 B(z) ds(z) M δ S[P ]( ) = (x) d x dz 2 s(P ) dM x dz P (x) Ω Ω

d2 s(z) dB(z) [(x)]2 dM x , + dz s(P ) dM x Ω dz 2 P (x) Ω 2

2

(6.60)

where (x) describes a small perturbation with Ω (x) dM x = 0. The first and second functional derivatives are given by

δS (x) dM x , δS[P ]() = (6.61) Ω δP (x)

δ2 S (x)(y) dM x dM y (6.62) δ 2 S[P ](2 ) = Ω δP (x)δP (y) (note that in general the second variation δ 2 S involves two different arguments 1 and 2 , see e.g. Sect. 5.1.8; in our context, however, we have 1 = 2 = , which is the perturbation of P ). From (6.58-6.60) it follows that dB(z) δS ds(z) = (6.63) δP (x) dz s(P ) dM x dz P (x) Ω

and δ2 S d2 B(z) ds(z) ds(z) = δP (x)δP (y) dz 2 s(P ) dM x dz P (x) dz P (y) Ω d2 s(z) dB(z) + δ(x − y) . dz s(P ) dM x dz 2 P (x) Ω

(6.64)

Expansibility The measure S is said to be expansible if states of the phase space Ω that are certainly not occupied by a system do not contribute to the entropy or information measured by S. Let suppΩ {P } denote the support of P , that is,

226


the subspace of Ω for which P is positive: suppΩ {P } = {x ∈ Ω|P (x) > 0}. For an expansible measure S we need to consider only the support of P : S[P ; Ω] = S[P ; Ω = suppΩ {P }] .

(6.65)

For example, an expansible measure is given by (6.56) with s(0) = 0 and B(0) = 0. Concavity A measure S is referred to as strictly concave if it satisfies for λ ∈ [0, 1] the inequality S[λP + (1−λ)P ] ≥ λS[P ] + (1−λ)S[P ] , (6.66) where the equal sign only holds in three cases: P = P , λ = 0, and λ = 1. Consequently, we have P = P ∧ λ ∈ (0, 1) : S[λP + (1−λ)P ] > λS[P ] + (1−λ)S[P ] .

(6.67)

In order to elucidate the meaning of the concavity inequality (6.66), we define a straight line Sline (λ) that connects the points (P , S[P ]) and (P, S[P ]), Sline (λ) = S[P ] + λ (S[P ] − S[P ]) ,

(6.68)

such that Sline (0) = S[P ] and Sline (1) = S[P ], see Fig. 6.1. The concavity inequality (6.66) states that Sline (λ) is smaller than S S[P + λ(P − P )] > Sline (λ) ,

(6.69)

for λ ∈ (0, 1) and P = P , see also Fig. 6.1.

S

S line 0 P/

λ

1 P

Fig. 6.1. Illustration of the concavity inequality (6.69)

From (6.66) the concavity inequality

δS S[P ] ≤ Slin [P, P ] = S[P ] + [P (x) − P (x)] dM x (x) δP Ω

(6.70)


227

S lin S

P/

P

Fig. 6.2. Illustration of the concavity inequality (6.70)

can be derived (see below), where the equal sign holds for P = P only. Slin [P, P ] denotes the linearization of S at the distribution P . Note that the concavity inequality (6.70) can be cast into the concise form S[P ] ≤ S[P ] + δS[P ](P − P ) .

(6.71)

We realize that if S is strictly concave, then the linearization of S is larger than S except for the “point” P at which the linearization is carried out, see Fig. 6.2. It can be immediately verified that (6.70) and (6.71) hold for P = P . By means of two different methods, we will show next how to obtain (6.70) for P = P : First Method to Derive (6.70) [168] Let us write (6.66) as S[P + λ(P − P )] − S[P ] > S[P ] − S[P ] , λ

(6.72)

with λ ∈ (0, 1). To evaluate (6.72), we use the concept of the directional functional derivative. Note that the directional derivative of an N -dimensional function f (x) in the direction of the vector h is given by f (x + λh] − f (x) = h · ∇f (x) . λ→0 λ lim

(6.73)

In a similarMvein, the directional functional derivative of an operator A[f ] = a(f (x)) d x in the direction of the function h(x) is given by

A[f + λh] − A[f ] δA (6.74) lim = h(x) dM x = δA[f ](h) . λ→0 λ δf (x)

228


That is, for the integral operator A the functional derivative in the direction h is given by the first variation δA[f ](h) of A at f for a perturbation h. Then, we can perform the limiting case

δS S[P + λ(P − P )] − S[P ] = [P (x) − P (x)] dM x lim (6.75) λ↓0 λ δP (x) (hint: use the identifications A → S, f → P , and h → P − P ). Substituting (6.72) in the left-hand side of (6.75), we obtain (6.70). Second Method to Derive (6.70) Our departure point is the functional R(λ; P , P ) = λ (S[P ] − S[P ]) − S[P ] + S[P + λ(P − P )] ,

(6.76)

for λ ∈ [0, 1]. Note that R satisfies R(0) = 0. Since S involves a differentiable scale function B and an integral kernel s that is differentiable for λ ∈ (0, 1) and P > 0, the functional R is differentiable with respect to λ for λ ∈ (0, 1) and P > 0. That is, limλ→0+ dR(λ)/dλ exists. Furthermore, we can read off from (6.67) that the inequality R(λ) > 0 for λ > 0 and P = P holds. From R(0) = 0 and R(λ) > 0 for λ > 0 and P = P it follows that limλ→0+ dR(λ)/dλ > 0 for P = P . Differentiation of (6.76) with respect to λ in the limiting case λ → 0+ for P = P yields dR(λ) S[P + λ(P − P )] − S[P ] = S[P ] − S[P ] + lim λ→0+ λ→0+ dλ λ = S[P ] − S[P ] + δS[P ](P − P ) , (6.77)

0 < lim

which is equivalent to (6.70). Implications of Concavity As discussed in Sect. 4.7.2 every concave entropy measure induces a semipositive definite Kullback measure. Furthermore, as discussed in Sect. 4.2 for concave entropy measures with δ 2 S < 0 stationary distributions always correspond to maximum entropy distributions. Extensivity, Nonextensivity, and Composability Let us consider two statistically independent continuous random variables X ∈ Ω and Y ∈ Ω that are distributed according to the probability densities P (x) = δ(x − X) and P (y) = δ(y − Y). A composed system described by the vector (X, Y) is given by the joint probability density P (x, y) = P (x)P (y). If the entropy or information of the composed system equals the sum of the entropy or information of the single systems like


S[P P ; Ω = Ωx Ωy ] = S[P ; Ωx ] + S[P , Ωy ] ,

229

(6.78)

then the measure S is said to be extensive [625] (see also Sect. 6.2.2). If we cannot add up the single-system entropy values in order to compute the entropy of the two-variable system, we say, S is nonextensive: S[P P ; Ω = Ωx Ωy ] = S[P ; Ωx ] + S[P , Ωy ] .

(6.79)

If S(P P ) can be computed from the measures S(P ) and S(P ) of the single systems, then we refer to S as a composable measure [587]. In this case, S[P (x, y)] can be computed from S[P ] and S[P ] and a symmetric function ˜ v) = G(v, ˜ u) like G(u, ˜ S[P P ; Ω = Ωx Ωy ] = G(S[P ; Ωx ], S[P , Ωy ]) .

(6.80)

On a Fundamental Entropy and Information Measure Let us consider now an entropy and information measure of the form (6.56) that is described by

M s[P (x)] d x , S[P ] = B Ω

s(z) ∈ C 0 ([0, ∞)), s(z) ∈ C ∞ ((0, ∞)) , s(0) = 0, z ∈ [0, 1] : s(z) ≥ 0 , B(z) ∈ C ∞ (Ωcod ), z ∈ Ωcod :

d2 B(z) 0, z ∈ Ωcod : 2 2 dB(z ) dB(z ) d s(z) d s(z) 0 ∨ >0 ∧ f (x0 ) + (x − x0 )df (x0 )/dx) [79]. As far as the entropy kernel s(z) is concerned, we have z = z0 , z0 ∈ (0, 1], z ∈ [0, 1] : s(z) − s(z0 ) − (z − z0 )

ds(z0 ) > 0. dz
0 :

N

s(pi ) >
0. From d2 s(z)/dz 2 < 0 and (6.89) it follows N N for z = i s(pi ) and z = i=1 s(pi ) + i=1 (pi − pi )ds(pi )/dpi that z > z . From dB(z)/dz > 0 it then follows that B(z) < B(z ), that is, we have 7 6N 7 6N N ds(pi ) . s(pi ) < B s(pi ) + (pi − pi ) {pi } = {pi }, pi > 0 : B dpi i=1 i=1 i=1 (6.90) < 0. Next, let us first consider the case d2 s(z)/dz 2 > 0 and dB(z)/dz Now, from d2 s(z)/dz 2 > 0 and (6.89) it follows for z = s(p ) and i i N N z = i=1 s(pi ) + i=1 (pi − pi )ds(pi )/dpi that z < z . From dB(z)/dz > 0 it then follows that B(z) < B(z ), that is, we obtain (6.90) again. The righthand side of (6.90) can be evaluated by means of the inequality (6.88). We put N N ds(pi ) s(pi ) + (pi − pi ) , z= dpi i=1 i=1 z0 =

N

s(pi ) ,

i=1 N

6 ⇒B

s(pi )

i=1 6N

0 : 6N 7 6N 7 dB(z) B s(pi ) < B s(pi ) + dz z0 =N i=1 i=1

i=1

N s(pi ) i=1

(pi − pi )

ds(pi ) , dpi (6.92)

which is equivalent to the concavity inequality (6.86). 6.4.2 Examples In this section we will present some entropy and information measures S that have found applications in various disciplines. Our emphasis will be on

232


the properties of these measures such as extensivity and concavity. We will examine some of these properties by means of probability distributions of discrete random variables. In these cases, probability distributions will be described by means of a set of probabilities pi with i = 1, . . . , N , pi ∈ [0, 1], N and i=1 pi = 1. Boltzmann Entropy Before we give the definition of the Boltzmann entropy, we highlight a property of the function f (x) = x ln x which occurs in the definition of the Boltzmann entropy. The function f (x) is not defined at x = 0: ln x −∞ f (x) = x ln x = . (6.93) ⇒ f (0) = 1 ∞ x However, using the rule of l’Hopital, we see that the limit value f (x → 0) exists: 1 ln x x lim f (x) = lim = − lim x = 0 . (6.94) = lim 1 x→0 x→0 1 x→0 x→0 − 2 x x For this reason, the domain of definition of the function f (x) = x ln x can be extended from x ∈ (0, ∞) to x ∈ [0, ∞) in such a way that we obtain a continuous function for x ∈ [0, ∞). To this end, the expression x ln x will be interpreted in what follows as x ln x for x > 0 [x ln x] = . (6.95) 0 for x = 0 The Boltzmann entropy is defined by

B S[P ] = SB [P ] = − P (x) ln P (x) dM x .

(6.96)

Ω

The entropy kernel reads s(z) = −z ln z and is a strictly concave function: d2 z/dz 2 = −1/z < 0 for z > 0. Furthermore, we have B(z) = z, s(0) = 0, s(z) ∈ C 0 ([0, ∞)), and s(z) ∈ C ∞ ((0, ∞)). Therefore, the Boltzmann entropy is continuous, differentiable, expansible, and strictly concave. Furthermore, for two statistically-independent random variables X ∈ Ωx and Y ∈ Ωy distributed according to P and P the Boltzmann entropy BS satisfies

B S(P P ) = − P (x)P (y) ln[P (x)P (y)] dM x dM y Ωx

Ωy

=− Ωx

Ωy

− Ωx

P (x)P (y) ln P (x) dM x dM y

Ωy

= S[P ] + BS[P ] . B

P (x)P (y) ln P (y) dM x dM y (6.97)


233

Consequently, the Boltzmann entropy is extensive. Note that as indicated in (6.96) we will use two different symbols for the Boltzmann entropy, namely, B S[P ] and SB [P ]. In particular, we will use the notation SB [P ] in the context of the second variation δ 2 SB . The Boltzmann entropy can in particular be used to describe the entropy of many-body systems that are in or close to thermodynamic equilibrium and are studied by means of their particle distribution functions (µ-space description) [48, 348, 432, 490, 576, 625]. The functional S = − ΩΓ P (x) ln P (x) dMΓ x can also be applied to describe systems with respect to the Γ -space and is then referred to as the Gibbs entropy [89, 97, 348, 625]. In this case, the vector x is composed of the vectors xi of the particles i = 1, . . . , N0 like x = (x1 , . . . , xN0 ) and the Γ -space ΩΓ is given by ΩΓ = Ω N0 , where Ω is the phase space of a single particle. Finally, the func tional S = − ΩΓ P (x) ln P (x) dMΓ x can be used to measure the disorder of systems that operate far from thermal equilibrium. In this case S is regarded as the Shannon information measure [261, 309, 310, 348, 509, 518, 625]. For a summary see Table 6.1. Table 6.1. Applications of the functional S = −

µ-space Γ -space

P ln P dΩ

Close to thermal equilibrium

Far from thermal equilibrium

Boltzmann Gibbs

– Shannon

Entropy for Fermions and Bosons Many particle systems composed of fermions and bosons can be described by means of the mean occupation number ρi of their energy levels i. The mean occupation number ρi describes how many particles of a system composed of N0 particles on the average occupy an energy level i with energy i . The phase space is given by Ω = {1 , . . . .N }. If the energy levels are not degenerated, the quantum mechanical entropy reads S(ρ1 , . . . , ρN ) = −

FD,BE

N i=1

ρi ln ρi ∓

N

(1 ∓ ρi ) ln(1 ∓ ρi ) ,

(6.98)

i=1

where the upper sign holds for fermions and the lower sign for bosons [9, 232, 238, 318, 340, 346, 359, 373, 490, 619]. Note that in the case of fermions the maximal mean occupation number ρi equals unity, that is, we have the

234


constraint ρi ≤ 1. The reason for this is that in the case of fermions an energy level i cannot be occupied by more than one particle. Note also that the Fermi entropy (6.98) also describes the entropy of the Fermi quasi-particles that occur in the BCS theory of superconductivity [464]. In line with the stochastic description involving discrete energy levels, a classical stochastic description for fermions and bosons can be obtained in the case of continuous energy levels. Let ∈ Ω describe the energy of a Fermi or Bose particle or subsystem. Let ρ() denote the occupation number density of the energy . Then, in analogy to (6.98) we define the entropy measure

FD,BE S[ρ] = − ρ() ln ρ() d ∓ [1 ∓ ρ()] ln[1 ∓ ρ()] d . (6.99) Ω

Ω

In analogy to the constraint ρi ≤ 1, for fermions we require ρ ≤ 1 [377]. The entropy (6.99) involves a linear entropy scale function B(z) = z and an entropy kernel s(z) = −z ln z ∓ (1 ∓ z) ln(1 ∓ z) . (6.100) The derivative of s(z) reads ds z 1 ∓1 = − ln = ln z 1∓z dz and is invertible:

ds dz

−1 (z) =

1 . exp{z} ± 1

(6.101)

(6.102)

The kernel satisfies s(0) = 0 and d2 s −1 0, r = 1 ⎪ ⎨ 1 − r ln R i=1 Sr (p1 , . . . , pN ) = . N ⎪ ⎪ ⎪ ⎪ p ln p , for r = 1 − i i ⎩ i=1

(6.112) In the continuous case, the Renyi measure reads ⎧

1 ⎪ r M ⎪ ⎨ [P (x)] d x , for r > 0, r = 1 ln R Ω

r Sr [P ] = 1 − . ⎪ ⎪ P (x) ln P (x) dM x , for r = 1 ⎩− Ω

(6.113) The Renyi measure is a one-parametric information measure. The parameter value r = 1 requires particular attention. The Renyi measure for r = 1 can be regarded as a function f (r) involving the function g(r) (with g = [pi ]r r M or g = P d x) as shown in (6.114). For r = 1 the function f (r) is not defined: ln g(r) 0 f (r) = , g(1) = 1 ⇒ f (1) = . (6.114) 1−r 0 For this reason, in (6.112) and (6.113) the case r = 1 is treated separately. Due to this supplementary definition, the Renyi measure is continuous with respect to the parameter r at r = 1. This property can be proven as follows. First, we write [pi ]r as pi exp{(r − 1) ln pi } and expand the exponential function into its Taylor series. Then, we expand the logarithmic function ln(1+x) into its Taylor series. Thus, we obtain 6 6 7 7 N N 1 1 R ln 1 − 1 − ln 1 − 1 − = Sr = [pi ]r pi e(r−1) ln pi 1−r 1−r i=1 i=1 6 7 N N ∞ n 1 (r − 1) n ln 1 + (r − 1) [ln pi ] = pi ln pi + pi 1−r n! n=2 i=1 i=1 6 7m ∞ N N ∞ (r − 1)n 1 m+1 1 n (r − 1) = (−1) pi ln pi + pi [ln pi ] 1−r m=1 m n! n=2 i=1 i=1 =−

N i=1

pi ln pi +

N i=1

pi

∞ (−1)n (1 − r)n−1 [ln pi ]n n! n=2 Y1 (r)


237

6

7m

N N ∞ ∞ (r − 1)n 1 m+1 1 (r − 1) + (−1) pi ln pi + pi . [ln pi ]n n! 1−r m=2 m n=2 i=1 i=1 Y2 (r) (6.115)

In the limit r → 1 the expressions Y1 and Y2 vanish. Consequently, we obtain lim Sr (p1 , . . . , pN ) = − R

r→1

N

pi ln pi = BS(p1 , . . . , pN ) .

(6.116)

i=1

Equation (6.116) states that in the limit r → 1 the Renyi measure reduces to the Boltzmann entropy. The scaling function B(z) satisfies ln z ⇒ 1−r 1 d2 B −1 dB = > 0, 0 . (6.117)

The kernel s(z) satisfies s(z) = z r ⇒

d2 s = r(r − 1)z r−2 < 0 for r ∈ (0, 1), z > 0 . dz 2

(6.118)

Consequently, the Renyi measures is a strictly concave measure in the pa0 rameter range r ∈ (0, 1]. Furthermore, we have s(0) = 0, s(z) ∈ C ([0, ∞)), s(z) ∈ C ∞ ((0, ∞)). The expressions i pri and Ω [P (x)]r dM x are larger than zero for any distribution {pi } and probability density P ∈ C 0 (Ω) due to the N normalization conditions i=1 pi = 1 and Ω P (x) dM x = 1. Therefore, the co-domain Ωcod is given by Ωcod = (0, ∞). We have B(z) ∈ C ∞ (Ωcod ). In view of these properties, we conclude that the Renyi measure is continuous, differentiable and expansible for r ∈ (0, 1]. Given two statistically independent random variables X and X described by the distributions {pi }N i=1 and the Renyi measure of the joint distribution p = p p satisfies {pi }N i,k i i=1 k N

1 ln = [pi pk ]r 1−r i=1 k=1 ⎫ ⎧ N N N N ⎬ ⎨ 1 1 1 = [pi ]r · [pk ]r = [pi ]r + [pk ]r ln ln ln ⎭ 1−r 1−r ⎩ i=1 1−r i=1 N

Sr (p1 p1 , . . . , pN pN )

R

k=1

R

= Sr (p1 , . . . , pN ) +

Sr (p1 , . . . , pN )

R

That is, the Renyi measure is extensive.

k=1

.

(6.119)

238


Nonextensive Entropy Proposed by Tsallis A one-parametric entropy measure proposed by Tsallis [582, 587] is given by ⎧ N N 1 − i=1 [pi ]q [pi ]q − 1 ⎪ i=1 ⎪ ⎪ = , for q > 0, q = 1 ⎨ 1−q q−1 T Sq (p1 , . . . , pN ) = N ⎪ B ⎪ ⎪ pi ln pi , for q = 1 ⎩ S=− i=1

(6.120) for the discrete case and ⎧

1 ⎪ q M ⎪ ⎨ [P (x)] d x − 1 , for q > 0, q = 1 T Sq [P ] = 1 − q Ω ⎪ ⎪ P (x) ln P (x) dM x , for q = 1 ⎩ BS = − Ω

(6.121) for the continuous case. The measure TSq for q = 1 can be written in terms of the functions f (q) and g(q) (with g = [pi ]q or g = P q dM x) as shown in (6.122). We realize that f (q) is not defined at q = 1: g(q) − 1 0 f (q) = , g(1) = 1 ⇒ f (1) = . (6.122) 1−q 0 For this reason, in the definition of TSq the case q = 1 is treated separately. The nonextensive entropy is continuous with respect to the parameter q at q = 1, which can be seen by writing TSq as T

Sq = =−

i

! " N ∞ pi −1 + e−(1−q) ln pi (1 − q)n−1 = [− ln pi ]n pi 1−q n! i=1 n=1

N i=1

pi ln pi +

N ∞

pi

n=2 i=1

(1 − q)n−1 [− ln pi ]n . n!

(6.123)

Consequently, in the limit q → 1 the nonextensive entropy reduces to the Boltzmann entropy: lim TSq (p1 , . . . , pN ) = −

q→1

N

pi ln pi = BS(p1 , . . . , pN ) .

(6.124)

i=1

The entropy TSq involves a linear scale function B(z) = z. The entropy kernel satisfies s(0) = 0, s(z) ∈ C 0 ([0, ∞)), s(z) ∈ C ∞ ((0, ∞)), and s(z) =

d2 s zq − z ⇒ 2 = −qz q−2 < 0 for q > 0, q = 1, z > 0 . 1−q dz

(6.125)


239

Consequently, for q > 0 the nonextensive entropy is continuous, differentiable, expansible, and strictly concave. Note that the entropy can also be defined for parameter values q < 0. In this case, Nhowever, the entropy measure is not expansible. Note that the expression i=1 [pi ]q can be expressed in terms of N

[pi ]q = 1 + (1 − q) TSq (p1 , . . . , pN ) .

(6.126)

i=1

Then, for two statistically independent random variables involving the dis N tributions {pi }N i=1 and {pi }i=1 and the joint distribution given by the probabilities pi,k = pi pk we get ⎡ ⎤ N N 1 T ⎣ Sq (p1 p1 , . . . , pN pN ) = [pi pk ]q − 1⎦ 1−q i=1 k=1 ⎡ ⎤ N N 1 ⎣ q q = [pk ] − 1⎦ [pi ] · 1−q i=1 k=1

" 1 ! {1 + (1−q) TSq (p1 , . . . , pN )} {1 + (1−q) TSq (p1 , . . . , pN )}−1 = 1−q = TSq (p1 , . . . , pN ) + TSq (p1 , . . . , pN ) (6.127) +(1 − q) TSq (p1 , . . . , pN ) TSq (p1 , . . . , pN ) . Equation (6.127) states that the entropy T Sq is nonextensive and composable. In particular, we have Sq (p1 p1 , . . . , pN pN ) = TSq (p1 , . . . , pN ) + TSq (p1 , . . . , pN ) ! " +G TSq (p1 , . . . , pN ), TSq (p1 , . . . , pN ) , (6.128)

T

with G(x, y) = (1 − q)xy. Note that in this chapter the nonextensive entropy by Tsallis will be used in the context of the µ-space descriptions of manybody systems. As such, the entropy has been discussed as an entropy measure both with regard to the µ-space and the Γ -space description of systems. Furthermore, the entropy has been discussed as in the context of information theory [8, 124, 598]. Sharma–Mittal Measure For a discrete phase space Ω = {m1 , . . . , mN }, the Sharma–Mittal entropy and information measure is defined by [520] SM

Sq,r (p1 , . . . , pN )

240


⎧ 1 2(q−1)/(r−1) ⎪ N r ⎪ ⎪1− i=1 [pi ] ⎪ ⎪ ⎪ , for q, r > 0, ⎪ ⎪ q−1 ⎪ ⎪ ⎪ N ⎪ 1 − exp (q−1) i=1 pi ln pi ⎪ ⎪ ⎪ ⎨ GSq = , for q > 0, q N q−1 = ⎪ ⎪ 1 ⎪ R ⎪ S = [pi ]r , for r > 0, r ln r ⎪ ⎪ 1 − r ⎪ ⎪ i=1 ⎪ ⎪ N ⎪ ⎪ ⎪ B ⎪ for q = 1, r S = − pi ln pi , ⎪ ⎩

q, r = 1 = 1, r = 1

.

= 1, q = 1 =1

i=1

(6.129) Accordingly, for a continuous phase space Ω, we get SM

Sq,r [P ] ⎧ 1 2(q−1)/(r−1) ⎪ ⎪ 1 − Ω [P (x]]r dM x ⎪ ⎪ ⎪ , for q, r > 0, ⎪ ⎪ ⎪ q−1 ⎪ ⎪ N ⎪ M ⎪ P (x) ln P (x)d x 1 − exp (q−1) ⎪ i=1 Ω ⎪ ⎨ GSq = , q−1 = ⎪ for q > 0, q ⎪ ⎪

⎪ ⎪ 1 ⎪ R ⎪ [P (x)]r dM x , for r > 0, r Sr = ln ⎪ ⎪ ⎪ 1 − r Ω ⎪ ⎪ ⎪ ⎪ ⎩ BS = − P (x) ln P (x) dM x , for q = 1, r

q, r = 1

= 1, r = 1

.

= 1, q = 1 =1

Ω

(6.130) For q = r the Sharma–Mittal measure is equivalent to the entropy TSq : SM

Sq,r=q = TSq .

(6.131)

The SMSq,r measure includes as special cases the Renyi measure, the nonextensive entropy TSq , the Boltzmann entropy and the one-parametric measure G Sq , see Fig. 6.3. The measure GSq will be referred to as Gaussian entropy. The two-parametric measure SMSq,r is continuous with respect to its parameters q and r at q = 1 and r = 1. Let us first investigate the case q = 1 and r → 1. For q = 1 and r = 1, the Sharma–Mittal measure can be written as N q−1 r 1 − exp ln [pi ] r − 1 i=1 1 − exp (1 − q) RSr SM Sq,r = = . (6.132) q−1 q−1 Since the Renyi information measure reduces in the limit r → 1 to the Boltzmann entropy and the measure GSq basically corresponds to an exponential


241

Gaussian entropy

q

y

se lli a Ts

p ro nt

Renyi entropy 1

0 0

r

1 Boltzmann entropy

Fig. 6.3. Concavity and limiting cases of the two-parameter entropy the parameter region colored grey the entropy is strictly concave

SM

Sr,q . In

function with the Boltzmann entropy as its argument, we realize that the limiting case 1 − exp (1 − q) lim RSr r→1 q = 1 : lim SMSq,r = (6.133) = GSq r→1 q−1 holds. Next, let us consider the limiting case q = 1 and r → 1. By definition, for q = 1 the Sharma–Mittal measure is equivalent to the Renyi measure. From our considerations on the Renyi measure, it follows that in the limit q = 1, r → 1 the measure SMSq,r is continuous again: Sq=1,r = RSr ⇒

SM

lim

r→1

SM

Sq=1,r = BS .

(6.134)

Now, let us consider the limiting case q → 1 and r = 1. To this end, we write Sq,r as ∞ 1 − exp (1 − q) RSr (−1)n (q−1)n−1 !R "n SM Sq,r = Sr . = RSr + q−1 n! n=2 (6.135) Then, we have (6.136) r = 1 : lim SMSq,r = RSr .

SM

q→1

We proceed by considering the case q → 1 and r = 1. In this case, we cast the measure GSq into the form

242


∞ 1 − exp (1 − q) BS (−1)n (q−1)n−1 !B "n = BS + S . Sq = n! q−1 n=2

G

(6.137)

Then, the limiting cases lim GSq = BS ,

q→1

lim

Sq,r=1 = lim GSq = BS

SM

q→1

q→1

(6.138)

hold. Finally, we consider the limiting cases q → 1, r → 1 and r → 1, q → 1. Then, we have SM lim lim Sq,r = lim RSr = BS , (6.139) r→1 q→1 r→1 9 : lim lim SMSq,r = lim GSq = BS . (6.140) q→1

r→1

q→1

For q = 1 the Sharma–Mittal measure is equivalent to the Renyi measure and, therefore, in this parameter regime SMSq,r is continuous, differentiable, and expansible. For q = 1 and r = 1 the scaling function B and the kernel s is given in (6.141) (see below). For q = 1 and r = 1 the scaling function B and the kernel s is given in (6.142) (see below). In both cases B and s satisfy s(0) = 0, s(z) ∈ C 0 ([0, ∞)), s(z) ∈ C ∞ ((0, ∞)), and B(z) ∈ C ∞ (Ωcod ) with Ωcod = (0, ∞), which implies that for q = 1 the Sharma–Mittal measure is continuous, differentiable, and expansible, again. As for the concavity of SM Sq,r , for q = 1 we are dealing with the Renyi measure. Therefore, SMSq,r is strictly concave for q = 1 and r ∈ (0, 1]. Next, let us explore the case q = 1. First, we consider the parameter range given by q > r and r ∈ (0, 1). Then, we have q > r, r ∈ (0, 1) : B(z) =

1 − z (q−1)/(r−1) , s(z) = z s , q−1

d2 s = r(r − 1)z r−2 < 0 , dz 2 dB 1 (q−r)/(r−1) z >0, = dz 1−r d2 B r − q (q−2r+1)/(r−1) = z 1, r = 1 : B(z) = 1 d2 s =− 0 , dz d2 B = (1 − q) exp{(1 − q)z} < 0 . dz 2

243

(6.142)

Again, we conclude that we are dealing with a strictly concave measure. Finally, we examine the parameter range q > r > 1. Then, we get q > r > 1 : B(z) =

1 − z (q−1)/(r−1) , s(z) = z s , q−1

d2 s = r(r − 1)z r−2 > 0 , dz 2 dB 1 (q−r)/(r−1) 0 ⇒ SMSq,r strictly concave. (6.144) This finding is consistent with the fact that on the diagonal q = r of the parameter space (q, r) we have the strictly concave entropy TSq , see also Fig. 6.3. In closing our investigation of the Sharma–Mittal measure, let us examine whether or not SMSq,r is an extensive measure. First, we note that for q = 1 and r = 1 the relation 7(q−1)/(r−1) 6N r [pi ] = 1 + (1 − q) SMSq,r (p1 , . . . , pN ) (6.145) i=1

holds. Consequently, one obtains ⎛⎡ ⎞ ⎤(q−1)/(r−1) N N 1 ⎜⎣ ⎟ SM Sq,r (p1 p1 , . . . , pN pN ) = [pi pk ]r ⎦ − 1⎠ ⎝ 1−q i=1 k=1

⎛

6

N 1 ⎜ q = [pi ] ⎝ 1−q i=1

7(q−1)/(r−1) ⎡ ⎣

N

⎤(q−1)/(r−1) [pk ]q ⎦

⎞ ⎟ − 1⎠

k=1

{1 + (1−q) SMSq,r (p1 , . . . , pN )} {1 + (1−q) SMSq,r (p1 , . . . , pN )}−1 1−q SM SM Sq,r (p1 , . . . , pN ) + Sq,r (p1 , . . . , pN ) = +(1−q) SMSq,r (p1 , . . . , pN ) SMSq,r (p1 , . . . , pN ) . (6.146) =

244


Likewise, for q = 1 and r = 1, we get exp (1−q) BS(p1 , . . . , pN ) = 1 + (1 − q) GSq (p1 , . . . , pN )

(6.147)

and 1 exp (1−q) BS(p1 p1 , . . . , pN pN ) − 1 1−q !B " 1 exp (1−q) S(p1 , . . . , pN ) + BS(p1 , . . . , pN ) − 1 = 1−q exp (1−q) BS(p1 , . . . , pN ) exp (1−q) BS(p1 , . . . , pN ) − 1 = 1−q G {1 + (1−q) Sq (p1 , . . . , pN )} {1 + (1−q) GSq (p1 , . . . , pN )}−1 = 1−q G G = Sq (p1 , . . . , pN ) + Sq (p1 , . . . , pN ) +(1−q) GSq (p1 , . . . , pN ) GSq (p1 , . . . , pN ) . (6.148) Sq (p1 p1 , . . . , pN pN ) =

G

From (6.146) and (6.148), we can read off that for q = 1 the Sharma–Mittal measure is nonextensive. In addition, SMSq,r is composable and satisfies (6.80) with G(x, y) = (1 − q)xy. For q = 1 the measure SMSq,r reduces to the Renyi measure and, therefore, is extensive. The power of the Sharma–Mittal measure lies in its unifying character. It includes the Renyi measure and the entropy TSq as special cases. Finally, note that there is also a three-parametric generalization of the Sharma–Mittal measure [136]. Average Information Measure We consider the measure Sψ (p1 , . . . , pN ) = ψ −1

A

A

Sψ [P ] = ψ

−1

N

pi ψ(− ln pi )

,

i=1

P (x) ψ[− ln P (x)] d x , M

Ω

ψ ∈ C ∞ (lR), lim [e−z ψ(z)] = 0, z ∈ lR : z→∞

dψ > d2 ψ > 0 , (6.149) dz < dz 2
0 and x ψ(− ln x) = 0 for x = 0. In particular, the limit x ↓ 0 yields ! " (6.150) lim [x ψ(− ln x)] = lim e−z ψ(z) = 0 . x↓0

z→∞

The scaling function B and the kernel s are given by


s(z) = zψ(− ln z), B(z) = ψ −1 (z) . They satisfy s(0) = 0, s(z) ∈ C 0 ([0, ∞)), s(z) ∈ C ∞ ((0, ∞)), and d2 s 1 dψ d2 ψ dz 2 z du −1 dB dψ >0 , = < du dz z=ψ(u) d2 B 0 is a constant. Note that empirical laws of this form abound in physics. For example, Fick’s law states that the flux of particles is proportional to the concentration gradient, Fourier’s law states that the flux of the heat energy is proportional to the temperature gradient and, finally, Ohm’s law tells us that electric currents are proportional to gradients of electric potentials [395]. In the context of linear nonequilibrium thermodynamics, we have expressed relations of this kind by means of (4.40) and (4.43): the thermodynamic current Jth is proportional to the gradient of the “thermodynamic potential” δF/δP or the chemical potential µ. State Equation of Polytropic Gases Our third and final ingredient is the state equation of polytropic gases ν p ρ = . (6.161) p ρ Equation (6.161) can be used to determine p as a function of ρ provided that we have information about a reference state with p and ρ . That is, from (6.161) it follows that p(ρ) = Cρν holds with C = p /[ρ ]ν .

6.5 Examples and Applications

249

Porous Medium Equation Taking (6.159-6.161) together, we obtain the porous medium equation ∂ ρ(x, t) = Q∆ρ(x, t)q , ∂t

(6.162)

with Q = νcp [ρ ]−ν /[ω(ν + 1)] and q = ν + 1. T

Sq -Entropy Fokker–Planck Equation Let M0 = Ω ρ(x) dM x denote the number of particles or the total mass of the system described by ρ. In order to interpret (6.162) as a Fokker–Planck equation we put P (x) = ρ(x)/M0 , replace QM0q−1 by Q and thus obtain ∂ P (x, t; u) = Q∆P q . ∂t

(6.163)

Equation (6.163), in turn, can be interpreted as the entropy Fokker–Planck equation (6.5) for the entropy (6.121). In fact, substituting the entropy TSq into (6.5) for I = 0, U0 = 0, and Mik = δik gives us (6.163). Barenblatt–Pattle Solutions In the univariate case, (6.163) reads ∂ ∂2 P (x, t; u) = Q 2 P q . ∂t ∂x

(6.164)

For (6.164) exact time-dependent solutions can be derived [34, 38, 329, 395, 467, 470]. For probability densities that are subjected to natural boundary conditions and correspond to delta distributions at time t = t0 , we get ⎤1/(1−q) ⎡ 1/(1+q) ⎥ ⎢ 1 1 ⎥ , ⎢ P (x, t; δ(x − x0 )) = D0 ⎣ t−t0 C0 (x − x0 )2 ⎦ 1+ (1 − q) 2 [t − t0 ]2/(1+q) (6.165) for q ∈ (0, 1). For q = 1 we deal with Wiener processes described by P (x, t; δ(x − x0 )) = P (x, t|x0 , t0 ; δ(x − x0 )) with P (x, t|x0 , t0 ; δ(x − x0 )) defined by (3.114) and K(t, t0 ) = Q(t − t0 ), m = 1, see Sect. 3.9.4. For q > 1 we obtain ⎡ ⎤1/(q−1) P (x, t; δ(x − x0 )) = D0

1 t−t0

⎥ 1/(1+q) ⎢ 2 ⎢ ⎥ ⎢1 − C0 (q − 1) (x − x0 ) ⎥ ⎢ ⎥ 2/(1+q) 2 [t − t0 ] ⎣ ⎦

,

Y (x, t) > 0 (6.166)

250


provided that the expression Y (x, t) is smaller than unity. For Y (x, t) ≥ 1 we put P (x, t; δ(x − x0 )) = 0. That is, we are dealing with a cut-off distribution. For the sake of convenience, we introduce the operator {·}+ : g(x, t) → h(x, t) defined by h(x, t) = {g(x, t)}+ = max[g(x, t), 0] . (6.167) That is, {·}+ maps real functions onto semi-positive real ones. Then, (6.165) and (6.166) can be summarized as P (x, t; δ(x − x0 )) = 71/(q−1) 1/(1+q) 6 C0 1 (x − x0 )2 1− . (6.168) D0 (q − 1) t − t0 2 [t − t0 ]2/(1+q) + The coefficients D0 and C0 are given by "−1/(1+q) ! , D0 = 2Qq(1 + q)[zq ]2 " 1! −2/(1+q) 2Qq(1 + q)[zq ]1−q , C0 = 2

(6.169)

where zq is defined in Table 6.3. For x0 = 0 the solution (6.168) is often called the Barenblatt–Pattle solution [38, 467]. Anomalous Diffusion It has been shown that for q = 1 the nonlinear diffusion equation (6.164) describes anomalous diffusion processes. To this end, the exact time-dependent solutions (6.168) [591], scaling arguments [99], and Ito–Langevin equations [66] have been used. The observation of anomalous diffusion is in line with the general property of entropy Fokker–Planck equations derived in Sect. 6.2.2, namely, that entropy Fokker–Planck equations with nonextensive entropy measures such as TSq describe anomalous diffusion processes. In Sect. 6.5.3 we will show how to derive (6.168) and return to the issue of anomalous diffusion. Flows in Porous Media We would like to point out that there are several modifications of the porous medium equation that play a crucial role in the description of gas and fluid flows in porous media, see, for example, [17, 76, 395, 468, 465, 559, 634]. 6.5.2 TSq -Entropy Fokker–Planck Equation by Plastino and Plastino We may regard stochastic processes described by the porous medium equation as generalized Wiener processes. If so, we may raise the question whether or


251

not stochastic processes with nonvanishing drift terms, such as Ornstein– Uhlenbeck processes can be generalized in a similar manner. This question can be answered in the affirmative. To this end, we supplement (6.164) with a drift term that is linear with respect to P . Thus, we obtain the nonlinear Fokker–Planck equation ∂ ∂ ∂2 P (x, t; u) = − h(x)P + Q 2 P q , ∂t ∂x ∂x

(6.170)

for x ∈ Ω = lR suggested by Plastino and Plastino [484]. Note that in [484] the diffusion term reads ∂ 2 P 2−˜q /∂x2 . Equation (6.170) corresponds to the diffusion form of the entropy Fokker–Planck equation (6.4) for the entropy T Sq , which can be verified by substituting TSq given by (6.121) into (6.46). Stationary Solutions If we evaluate the entropy kernel (6.125) of TSq , we find ds/dz = (qz q−1 − 1)/(1 − q) and 1/(1−q) −1 ds q (z) = . (6.171) dz 1 + (1 − q)z From (6.6) it then follows that the stationary solution of (6.170) is described by 1/(q−1) 1 + (1 − q)(U0 (x) − µ)/Q Pst (x) = ; (6.172) q + x for q = 1 and U0 (x) = − h(x ) dx. For q = 1 we are dealing with a linear Fokker–Planck equation and the stationary probability density is given by the Boltzmann distribution of U0 (x). Equation (6.172) can alternatively be expressed as Pst (x) = Dst

1/(q−1) (1 − q) 1+ U (x) , q−1 0 + qQDst

(6.173)

with Dst = [(1 − (1 − q)µ/Q)/q]1/(q−1) . Linear Drift Force, Power Law Distributions, and Anomalous Diffusion For h(x) = −γx and γ > 0 we have ∂ ∂ ∂2 P (x, t; u) = γxP + Q 2 P q ∂x ∂x ∂t and the stationary solution is given by

(6.174)

252


–20

–10

x

10

20

0 –2 –4 –6 –8 ln P(x) –10

Fig. 6.4. Log-normal plot of the stationary solution Pst of (6.174). Diamonds: Pst computed from (6.194) with h(x) = −γx using the averaging method for selfconsistent Langevin equations. Solid line: exact solution (6.175). Parameters: γ = 0.1, Q = 1.0, q = 0.8 (L = 20000, ∆t = 0.3, 2[∆x]2 = 0.1, wn via Box–Muller)

–3

–2

sgn(x) ln |x| 1 2

–1

3

0 –2 –4 ln P(x) –6 –8 –10

Fig. 6.5. Graphs shown in Fig. 6.4 are depicted here as log-log plots. As predicted by (6.176), we obtain straight lines with slopes ±2/(1 − q) in the asymptotic limit. For comparison we have also depicted dotted lines with slopes ±2/(1 − q) [179]

6 Pst (x) = Dst

γ 2 1− q−1 (q − 1)x 2qQ Dst

71/(q−1) ,

(6.175)

+

for q = 1. For q = 1 we obtain the stationary solution of Ornstein–Uhlenbeck processes: Pst (x) ∝ exp{−γx2 /Q}. For q ∈ (0, 1) we are dealing with solutions that describe power laws in the asymptotic limit: 2 − 1 − q Pst (x) ∝ |x|

for |x| → ∞ ,

(6.176)


253

see Figs. 6.4 and 6.5. In contrast, for q > 1 we have cut-off distributions. The coefficient Dst = [ γ/ (2qQzq2 )]1/(1+q) can also be found in Table 6.4 as TDst . A transient solution of (6.174) is given by [191, 484, 591] 1/(q−1) 2 2 P (x, t; δ(x − x0 )) = D(t) 1 − [zq D(t)] (q − 1) (x − m(t)) , +

(6.177) with m(t) = x0 exp{−γ(t − t0 )} , 71/(1+q) 6 1 1 γ D(t) = . 2qQ [zq ]2 1 − exp{−(1 + q)γ(t − t0 )}

(6.178)

The variance K(t) of the solution (6.177) can be obtained. In particular, in the limiting case of a vanishing drift force (i.e., for γ = 0), we find that K(t) ∝ t2/(1+q)

(6.179)

(see (6.275) below). We have an anomalous diffusion for q = 1, see Figs. 6.6 and 6.7. A derivation of (6.175-6.179) will be given in Sect. 6.5.3. The transient solution (6.177) reduces in the limit q → 1 to the transient solution of an Ornstein–Uhlenbeck process given by P (x, t; δ(x − x0 )) = P (x, t|x0 , t0 ; δ(x − x0 )), with P (x, t|x0 , t0 ; δ(x − x0 )) defined by (3.114), see Sect. 3.9.5. Therefore, (4.37) can be regarded as a generalization of Ornstein– Uhlenbeck processes to systems characterized by the nonextensive entropy measure TSq . H-Theorem for h(x) For classical solutions of (6.170) we can apply the H-theorem of free energy Fokker–Planck equations, see Sect. 4.3. Accordingly, (6.170) describes relaxation processes with P (x, t; u) → Pst related to a decrease of the free energy measure F = UL − Q TSq . Let us demonstrate that the inequality dF/dt ≤ 0 holds for solutions of (6.170). The evolution of F [P ] can conveniently be determined by means of the corresponding generalized Kullback measure K[P, Pst ] [192]. More precisely, from (4.131) it follows that dF/dt = QdK/dt. Therefore, we will examine the time-dependent behavior of K[P, Pst ] rather than the evolution of F [P ]. Substituting S = TSq into (4.126) we obtain

1 T K[P, Pst ] = [Pst (x)]q dx + P (x) q[Pst (x)]q−1 − [P (x)]q−1 dx . (1−q) Ω Ω (6.180) By means of the generalized logarithm Lnq (z) =

z q−1 − 1 q−1

⇒

lim Lnq (z) = ln z ,

q→1

(6.181)

254


250 200 150 K 100 50 0

10

20

30 t

40

50

60

Fig. 6.6. Variance K(t) as a function of t. Diamonds: simulation of (6.195) using the averaging method for self-consistent Langevin equations. Solid line: exact solution K(t) ∝ t2/(1+q) given by (6.275). Dotted line: K(t) ∝ t. Parameters: Q = 1.0, q = 0.8 (L = 2000, ∆t = 0.3, 2[∆x]2 = 0.1, wn via Box–Muller)

5 4 ln K 3 2 1 0

1

2 ln t

3

4

Fig. 6.7. The graph t → K(t) shown in Fig. 6.6 is depicted here as a log-log plot. As predicted by (6.275), we obtain a straight line

the relation (6.180) can be expressed as

T T K[P, Pst ] = (1−q) Sq [Pst ] + P (x) {Lnq [P (x)] − qLnq [Pst (x)]} dx (6.182) Ω

(note that an alternative generalization of the logarithmic function has been proposed in [592]). From (6.182) we can read off that in the limit q → 1 the functional TK reduces to Ω P (z) ln {P (z)/Pst (z)} dz, that is, it recovers the Kullback measure based on the Boltzmann entropy. The first derivative of T K[P, Pst ] with respect to t reads


∂ P (x, t; u) dx . ∂t Ω (6.183) Substituting the entropy Fokker–Planck equation (6.170) into (6.183) and integrating by parts gives us

Q ∂P q d T ∂P dPst −h + dx , P [Pst ]q−2 K[P, Pst ] == q − [P ]q−2 ∂x dx P ∂x dt Ω (6.184) q d T K[P, Pst ] = (1−q) dt

255

[Pst (x)]q−1 − [P (x, t; u)]q−1

when assuming that the surface term arising from the partial integration vanishes. Using h(x)Pst (x) = Q d[Pst (x)]q / dx, (6.184) can be transformed into 2

d T 2 q−2 dPst q−2 ∂P −P K[P, Pst ] = −q Q P [Pst ] dx ≤ 0 , (6.185) dx ∂x dt Ω implying that the Kullback measure and Lyapunov functional TK is a nonincreasing function. The inequality d TK/dt ≤ 0, in turn, gives us dF [P ]/dt ≤ 0 (as argued above). H-Theorem for h(x) = −γx Let us now focus on the special case (6.174). Substituting the transient solution (6.177) and the corresponding stationary solution (6.175) into (6.180) yields γ 2 K[P (x, t; δ(x − x0 )), Pst ] = m (t) 2Q

q 1 q+1 q+1 q−1 (1+q)[Dst ] + (1−q)[Dst ] − 2[D(t)] + [D(t)]2 (3q−1)(1−q) (6.186)

T

(for details see the Appendix in [192]). Note that Dst denotes the stationary value of D(t), that is, we have Dst = D(t → ∞) = [ γ/ (2qQzq2 )]1/(1+q) (see Table 6.4). Note also that for solutions (6.177) the integrals involved in (6.180) diverge for q ∈ (0, 1/3] [192]. Consequently, the generalized Kullback measure (6.180) only applies to solutions (6.177) with q ∈ (1/3, 1). The functional (6.186) and the evolution of the normalization constant D(t) in (6.178) allow for several conclusions. Since D(t) is a positive and strictly monotonically decreasing function (i.e., we have D(t) > 0 and dD(t)/ dt < 0) with D(t → t0 ) → ∞, D(t → ∞) = Dst , and 0 ≤ t < ∞ : D(t) > Dst , we find lim TK[P, Pst ] =

t→t0

γ q(1 + q) [x0 ]2 + [Dst ]q−1 > 0 , 2Q (3q − 1)(1 − q) ≥0

>0

(6.187)


1st derivative of Lyapunov functional

256

Lyapunov functional

6 5 4 3

0

q=0.45 q=0.6

–10

–20

0.2

0.4

time

0.6

0.8

1

2 1

q=0.6 q=0.45

0

0.2

0.4

time

0.6

0.8

1

Fig. 6.8. Lyapunov functional TK given by (6.190) as a function of time for Q = γ = 1, m0 = 0, and different values of q: q = 0.45, q = 0.5, and q = 0.6 (from bottom to top). Inlet: First derivative of the Lyapunov functional TK computed from (6.191): q = 0.45, q = 0.5, and q = 0.6 (from top to bottom). Note that the first derivative c 2001, with permission is singular at t = 0, cf. also (6.191); reprinted from [192], from Elsevier

d T γ dm2 (t) 2q [D(t)]1+q −[Dst ]1+q dD(t) lim K[P, Pst ] = + < 0, t→t0 dt 2Q dt (3q − 1)[D(t)]3 dt ≤0

>0

0 and q, r = 1 by ⎡ ⎤

(q−1)/(r−1) 1 ⎣ SM ⎦ , 1− Sq,r = P r dx (6.206) q−1 Ω

1 SM P r dx , (6.207) Sq=1,r = RSr = ln 1−r Ω

1 SM 1 − exp (q−1) Sq,r=1 = GSq = P ln P dx . (6.208) q−1 Ω As shown in Sect. 6.4.2, the Sharma–Mittal entropy includes as special cases the entropy TSq and the Boltzmann entropy BS, which we list here for the sake of completeness:

1 T SM (P q − P ) dx , (6.209) Sq=r,r = Sq = 1−q Ω

SM Sq=1,r=1 = BS = − P ln P dx . (6.210) Ω

Substituting the entropy measures SMSq,r , RSr , TSq , and GSq into (6.46), we obtain the entropy Fokker–Planck equations

−1 2

R r ∂ R r ∂ R ∂ R P (x, t; u) = − h(x) P + Q P dx ( P ) , (6.211) 2 ∂t ∂x ∂x Ω ∂ T ∂ ∂ 2 q P (x, t; u) = − h(x) TP + Q 2 TP , (6.212) ∂t ∂x

⎤ ⎡∂x G G ∂ G ∂ ⎢ (q−1) Ω P ln P dx⎥ ∂ 2 G P (x, t; u) = − h(x) GP +Q⎣e ⎦ 2 P , ∂t ∂x ∂x


Gaussian entropy

q

Gaussian NLFPE

262

E FP NL o

Ts

li al

nt

se

y op

r

in

t as

l

-P

o in

st

a Pl

Renyi entropy

1 Renyi NLFPE 0 0 1/3

1

r

Boltzmann entropy linear Fokker-Planck Eq.

Fig. 6.12. Limiting cases of the two-parametric Sharma–Mittal entropy SM Sr,q and limiting cases of the Sharma–Mittal entropy Fokker–Planck equation (6.214) c 2000, with (NLFPE = nonlinear Fokker–Planck equation); reprinted from [191], permission from Elsevier

(6.213) q−r

2

SM r ∂ SM ∂ r−1 ∂ SM r P dx P , P (x, t; u) = − h(x) SMP +Q ∂x ∂x2 ∂t Ω (6.214) for t ≥ t0 . Figure 6.12 depicts the limiting cases RSr , TSq , and GSq of the entropy functional SMSq,r and the corresponding limiting cases (6.211-6.213) of the entropy Fokker–Planck equation (6.214) in the parameter-space (r, q). Note that the entropy Fokker–Planck equation (6.212) corresponds to the one discussed in the previous section. The evolution equations (6.211-6.214) can be used to define generalized Ornstein–Uhlenbeck processes and generalized Wiener processes related to the Sharma–Mittal entropy. To this end, we put h(x) = −γx for γ ≥ 0 and consider the entropy Fokker–Planck equations

−1 2

R r ∂ R ∂ R r ∂ P (x, t; u) = γ x RP + Q P dx P , ∂t ∂x ∂x2 Ω ∂ T ∂ ∂ 2 q P (x, t; u) = γ x TP + Q 2 TP , ∂t ∂x ∂x

(6.215) (6.216)


⎡ ∂ G ∂ ⎢ (q−1) P (x, t; u) = γ x GP + Q ⎣e ∂t ∂x ∂ SM ∂ P (x, t; u) = γ x ∂t ∂x

263

⎤

P lnG P dx ⎥ ∂ 2 ⎦ 2 ∂x

G Ω

G

P , (6.217)

q−r 2

r r−1 ∂ SM r SM SM P (x, t; u)+Q P dx P , ∂x2 Ω (6.218)

with r > 1/3, q > 0, and r, q = 1 .

(6.219)

The restriction on r will be explained below. We will study probability densities (·)P (x, t; u) = δ(x − X(t)) subjected to natural boundary conditions that describe a random variable X(t) ∈ Ω = lR for t ≥ t0 = 0. First, let us discuss the stationary case. Stationary Solutions It is convenient to introduce the functionals (·) U(t) : (·) P (x, t; u) → (·) U[(·) P ], which occur in the diffusion coefficients of (6.215-6.218). These functionals read

R r R U = P dx , (6.220) Ω T G

U = 1,

U = exp (1−q)

(6.221)

G G P ln P dx ,

(6.222)

Ω

SM

U =

q−r

SM r 1−r . P dx

(6.223)

Ω

We assume that (·) U(t) is finite and positive, which implies that we can write the entropy Fokker–Planck equations (6.215-6.218) as ∂ ∂ P (x, t; u) = γ x P + ∂t ∂x

∂2 ν Q ( P) , U(t) ∂x2

(6.224)

with (, ν) = (R, r), (, ν) = (T, q), (, ν) = (G, 1), and (, ν) = (SM, r). In the stationary case, the functionals (6.220-6.223) are positive constants, (·) Ust > 0. Consequently, the stationary solutions of (6.224) correspond to the stationary solution (6.173) of (6.170) for U0 (x) = −γx2 /2 when replacing q by ν and Q by Q/(·) Ust > 0. Thus, we obtain 6

Pst (x) =

Dst

bν Ust 1− (ν − 1)x2 ( Dst )ν−1

7 +

1 ν−1

,

(6.225)

264


for (, ν) = (R, r), (, ν) = (T, q), and (, ν) = (SM, r). For (, ν) = (G, 1) the entropy Fokker–Planck equation (6.224) can be regarded as a linear Fokker–Planck equation when G U(t) is considered as a time-dependent coefficient, which means that in the stationary case (i.e, for G U(t) = G Ust ) we are dealing with a Boltzmann distribution γ G Ust γ G Ust 2 G x . (6.226) Pst (x) = exp − 2πQ 2Q G Dst The factor bν is defined as bν = γ/(2νQ). We assume that the normalization constants (·) Dst are finite and positive. Since bν > 0, Ust > 0, and ν−1 ( Dst ) > 0, the probability densities (6.225) correspond to classical solutions for ν ∈ (0, 1) (i.e., we have Pst ∈ C ∞ ). For ν > 1 the probability densities (6.225) are continuous but not continuously differentiable at x = ± ( Dst )ν−1 /[(ν − 1)bν Ust ] and describe cut-off distributions. Returning to our objective to find the stationary solutions of the entropy Fokker–Planck equation (6.224), the normalization constants (·) Dst along with the functionals (·) Ust can be calculated from the conditions (6.220 6.223) and the normalization condition Ω (·) Pst dx = 1. The key step here is to use linear variable transformations ν form x = cy in order to express of the the integrals Ω (·) P dx = 1 and Ω (·) P dx by means of the constants zν and zνν listed in Table 6.3. The results obtained from this procedure are summarized in Table 6.4. Equations (6.225) and (6.226) in combination with Tables 6.3 and 6.4 provide a complete description of the stationary solutions of the (6.215-6.218) in the parameter range (6.219). Power Law Distributions For ν ∈ (1/3, 1) and large |x| the stationary distributions (6.225) decay for |x| → ∞ like 2 − 1 − ν . Pst (x) ∝ |x| (6.227) This means that we are dealing with power law distributions with an exponent δ = −2/(1 − ν) that is in the range (3, ∞). Cut-Off Distributions For ν > 1 and = G the stationary distributions (6.225) correspond to cut-off distributions. They are positive on the interval (−x∗ , x∗ ), where x∗ denotes the argument for which the curled bracket in (6.225) vanishes. That is, we have ( Dst )ν−1 . (6.228) x∗ = (ν − 1)bν Ust For |x| ≥ x∗ we have P st (x) = 0.


265

Table 6.3. Definition of the integrals zν and zνν . Representations in terms of Betaand Gamma-functions and limits for ν → 1 [191]

zν =

1

zνν =

1

|1 − ν|

zν =

zνν =

|1 − ν|

∞ 1 −∞

1 + sgn(1 − ν)y 2

∞ 1 −∞

1 2ν − 1 dy , ν > 0 , ν = 1 +

1 + sgn(1 − ν)y 2

ν 2ν − 1 dy , ν > 1 , ν = 1 + 3

⎧ 1+ν ⎪ ⎪ Γ ⎪ 9 : ⎪ 2(1 − ν) ⎪ 1 B 1, 1 + ν π ⎪ : for ν ∈ (0, 1) 9 ⎪ ⎪ 1−ν 2 2(1 − ν) = 1−ν 1 ⎪ ⎪ Γ ⎪ ⎪ 1−ν ⎪ ⎪ ⎨√ for ν → 1

π

⎪ ⎪ ⎪ ⎪ ⎪ ⎪ 9 : ⎪ ⎪ ⎪ 1 B 1, ν ⎪ ⎪ ν − 1 2 ν − 1 ⎪ ⎪ ⎪ ⎩

=

9

:

ν π ν − 1 for ν > 1 ν−1 3ν − 1 Γ 2(ν − 1) Γ

⎧ 3ν − 1 ⎪ ⎪ Γ ⎪ : 9 : 9 ⎪ 2(1 − ν) 1 ⎪ π 1 B 1 , 3ν − 1 ⎪ 9 : ,1 = for ν ∈ ⎪ ⎪ ν 1−ν 1−ν 2 2(1 − ν) 3 ⎪ ⎪ Γ ⎪ ⎪ 1−ν ⎪ ⎪ ⎨√ for ν → 1

π

⎪ ⎪ ⎪ ⎪ ⎪ ⎪ 9 : ⎪ ⎪ ⎪ 1 B 1 , 2ν − 1 ⎪ ⎪ ν−1 2 ν−1 ⎪ ⎪ ⎪ ⎩

zν 3ν − 1 1 = , ν> 3 zνν 2ν

=

9

:

2ν − 1 π ν − 1 for ν > 1 ν−1 5ν − 3 Γ 2(ν − 1) Γ

266


Table 6.4. Stationary values for

R

br zrr 3 = (zr )

bq (zq )2

G

D,

U, and the ratio

Dst

T

0

2rbr (3r − 1)(zr )2

Ust

γ 2πQ

GU

=

Ust / (Dst )ν−1

zrr = 2r zr 3r − 1

1

2 (zq )2 T Dst bq

9 st

U/ (D)ν−1 [191]

(zr )2 R r+1 Dst br

1

q+1

: 1−q γ 1+q 2πeQ

−

1 γ √ (q−1) 1+q e 2πQ 6 SM

br (zr )2

9

6 br = (zr )2

zrr zr

9

7 1 : q − r 1+q 1−r

r+1 (zr )2 SM Dst br

2 (zr )2 SM Dst br

7 1 : q − r 1+q 2r 1−r 3r−1

Border r = 1/3 In closing these considerations, we discuss the limiting case r ↓ 1/3. For ν = 1/3 and for large x, the integrand of zνν is proportional to 1/|x|, see Table 6.3. Consequently, the integral zνν diverges. For 0 < ν < 1/3 the integrand of zνν behaves for large x as 1/|x|m with m ∈ (0, 1), which again implies the divergence of the integral. Since zνν occurs in RDst and SMDst , the stationary solutions of the Renyi and Sharma–Mittal entropy Fokker–Planck equations (6.215) and (6.218) are not well-defined for 0 < r ≤ 1/3, respectively. There is no effect on the stationary solutions of Plastino–Plastino Fokker–Planck equation (6.216). However, tracing the entropy Fokker–Planck equation (6.216) back to the entropy functional TSq given by (6.209), we realize that the entropy TSq of the stationary solution (6.225) with (, ν) = (T, q) also diverges for 0 < q ≤ 1/3. For this reason, we require q > 1/3, as indicated by (6.219). Let us briefly discuss the situation in which the dashed line shown in Fig. 6.12 is approached from the right-hand side. In the case of the Renyi


(b)

P

x

(c)

P

(a)

q=1

0.5

4

q=2

x

(d) q=r

x

P

P

267

0.5

q=0.1 1 > r, q = 1 > r, q = r, and q < r. In detail we have (a) SMPst (x) for q = 2, (b) RPst (x) (q = 1), (c) TPst (x) (q = r), and d) SMPst (x) for q = 0.1; reprinted from c 2000, with permission from Elsevier [191],

r−1

, which is a meaentropy Fokker–Planck equation the ratio R Ust / R Dst sure of how fast the stationary solution (6.225) falls off at the origin, runs to infinity for r ↓ 1/3 (see Table 6.4), which means that for r ↓ 1/3 the stationary solution (6.225) of The Renyi entropy Fokker–Planck equation (6.215) converges to a delta distribution. For q > r, with the same reasoning, we can conclude that the stationary solutions of the Sharma–Mittal entropy Fokker– Planck equation (6.218) converge in the limit r ↓ 1/3 to delta distributions. In contrast, for q < r, the normalization constant SM Dst vanishes in the r−1

limit r ↓ 1/3 and, in turn, the ratio SM Ust / SM Dst converges to zero, see Table 6.4. Then, the stationary solution (6.225) converges to the uniform distribution. In addition, the Plastino–Plastino model (6.216) is not at all affected by the limit r ↓ 1/3 and yields a classical solution, that is, an infinitely differentiable function. These results are summarized in (6.229): ⎧ q>1 : SMPst → δ(x) ⎪ ⎪ ⎪ ⎪ : RPst → δ(x) ⎨q = 1 r ↓ 1/3 1 > q > r : SMPst → δ(x) . ⎪ T ∞ ⎪ q = r : P ∈ C (classical solution) ⎪ st ⎪ ⎩ q 0, C(t) > 0, and m(t) are time-dependent functions. Just as in the stationary case, for ν > 1 we regard the probability density (6.230) as a cut-off solution. The normalization of (6.230) determines the relation between D and C: 2 C(t) = 2 [zν D(t)] . (6.231) Using (6.231) and inserting the probability density (6.230) into (6.224), we obtain first order differential equations for D(t) and m(t) described by d 2νQ ν+2 [ D(t)] D(t) = γ D(t) − , dt U(t) d m(t) = −γ m(t) . dt

(6.232) (6.233)

Next, we express the functional U(t) in terms of D(t). Therefore, we substitute the probability density (6.230) together with (6.231) into the functionals (6.220), (6.221), and (6.223). We get "r − 1 zrr !R D(t) , zr T U(t) = 1 ,

R

SM

U(t) =

q−r !SM "r − q zrr 1−r . U(t) = D(t) zr

We can now eliminate the functional evolution equations for D(t) become

(6.234) (6.235) (6.236)

U(t) occurring in (6.232) and the

3 "3 [zr ] !R d R D(t) = γ RD(t) − 2νQ D(t) , dt zrr

(6.237)

"q+2 d T 2! D(t) = γ TD(t) − 2νQ [zq ] TD(t) , dt

(6.238)


d SM D(t) = γ dt

2

D(t) − 2νQ [zr ]

SM

269

q−r "q + 2 zr 1−r !SM D(t) . (6.239) zrr

For γ > 0 and P (x, 0; u) = u(x) = δ(x − x0 ), we can immediately solve the Bernoulli equations (6.237-6.239) as well as (6.233), which yields 6 R

D(t) = br

zrr 3

[zr ]

1 1 − exp{−2γt}

71 2

1 2rbr 1 2 , = (3r − 1)[zr ]2 1 − exp{−2γt}

6 T

D(t) = bq 6

SM

D(t) = br

and

1 2

[zq ]

1 1 − exp{−(1 + q)γt}

1 2

Kr,q [zr ]

7 1 1+q

1 1 − exp{−(1+q)γt}

(6.240)

,

7 1 1+q

(6.241)

,

m(t) = x0 e−γt ,

(6.242)

(6.243)

where Kr,q is given by q−r q−r 3r − 1 1−r zr 1−r = Kr,q = zrr 2r !√ "(1−q) 3r − 1 ⇒ Kl,l = 1 , Kr,q=1 = , lim Kr,q = e . r→1 2r

(6.244)

The limiting case limr→1 Kr,q listed in (6.244) can be found by rewriting the ratio zrr /zr as [{1 + (1 − r)(zr )2 x2 }+ ]r/(r−1)dx = ur (x)r dx and calculatr 1/(r−1) , which gives ing the limit limr→1 [zr /z! rr ]1/(1−r) " dx] √ = limr→1 [ ur (x) us the limiting case exp limr→1 ur (x) ln ur (x)dx = 1/ e along the lines of limr→1 SMSq,r = GSq , see Sect. 6.4.2. The probability densities (6.230) along with the relations (6.240-6.244), and (6.231) describe transient probability densities of generalized Ornstein–Uhlenbeck processes for initial delta distributions centered at x0 . Let us focus on the entropy Fokker–Planck equation (6.217) or alternatively on (6.224) for (, ν) = (G, 1). In what follows, we will demonstrate that (6.217) admits time-dependent Gaussian distributions (whence the label G). Using a notation similar to (6.230), we are looking for a solution of the form

270


G C(t) 2 (x − m(t)) . P (x, t; u) = D(t) exp − 2

G

G

(6.245)

Due to the normalization of the probability density (6.245), we find G

C(t) = 2

!√

"2 π GD(t)

(6.246)

(see (3.106)), which is also consistent with the limiting case ν → 1 of (6.231) (cf. also Table 6.3). Inserting the probability density (6.245) into (6.224), we again obtain dm/dt = −γ m and, in addition, the evolution equation "3 d G 2πQ !G D(t) = γ GD(t) − G D(t) . dt U(t)

(6.247)

Substituting (6.245) into the functional GU (see (6.222)) results in G

U(t) =

"1−q

√ q−1 !G e D(t) .

(6.248)

Finally, we insert the functional (6.248) into (6.247), which gives us

√ 1−q !G "q + 2 d G D(t) = γ GD(t) − 2πQ e D(t) . dt

(6.249)

Solving (6.233) and (6.249) for an initial delta distribution GP (x, 0; u) = u(x) = δ(x − x0 ) yields (6.243) and 1

√ 1 γ q−1 1+q G . e D(t) = 1 − exp{−(1+q)γt} 2πQ

(6.250)

In the limits q → 1 and r → 1 we obtain the time-dependent solution P (x, t; δ(x − x0 )) of an Ornstein–Uhlenbeck process given by P (x, t; δ(x − x0 )) = P (x, t|x0 , t0 ; δ(x − x0 )) with P (x, t|x0 , t0 ; δ(x − x0 )) described by (3.114), see Sect. 3.9.5. Evolution of Variances To classify the previously derived solutions into anomalous diffusion processes and normal diffusion we first derive a general expression for the processes, 2 variance K = X 2 − X of the probability densities in question. The first moment of the probability densities (6.230) and (6.245) equals m(t) and the variance GK of the Gaussian solution (6.245) is determined by G

K(t) =

1 . C(t)

G

(6.251)

For the probability density (6.230) a similar expression can be found,


271

Table 6.5. Definition of the integral zνσ . Representations in terms of Beta- and Gamma-functions, and limit for ν → 1 [191]

zνσ =

1

|1 − ν|

∞ −∞

3

y2

1

1 + sgn(1 − ν)y 2

1 2ν − 1 dy , ν > 1/3 , ν = 1 +

⎧ 3ν − 1 ⎪ ⎪ Γ 0 9 : 9 : ⎪ π ⎪ 2(1 − ν) ⎪ 1 ⎪ 9 : for ν ∈ 1 , 1 , 3ν − 1 B 3 = 1 ⎪ 3 3 2 2 1 ⎪ 2(1 − ν) 3 (1−ν) (1−ν) Γ ⎪ ⎪ ⎪ 1−ν ⎪ ⎪ ⎪ ⎨ zνσ =

1 √π

2 ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ 0 ⎪ 9 : ⎪ ⎪ 1 3, ν ⎪ ⎪ B 3 ⎪ 2 ν−1 ⎪ (ν − 1) ⎪ ⎩

K(t) = 2

zνσ zν

for ν → 1

1

= 2

:

ν π ν − 1 for ν > 1 (ν − 1)3 5ν − 3 Γ 2(ν − 1)

1 2 = C(t) 3ν − 1

9

Γ

1 , C(t)

(6.252)

with the integral zνσ defined in Table 6.5. Notice that for ν ∈ (0, ∞) the integral zνσ converges (diverges) if and only if zνν converges (diverges), because the integrands of zνν and zνσ have the same asymptotic behavior for |x| → ∞ (we can rewrite the exponent ν/(ν−1) as 1/(ν−1)+1). Furthermore, note that by exploiting the definition of the Gamma-function (i.e., Γ (x + 1) = xΓ (x)), we can find simple expressions for the ratios zνσ /zν , zνσ /zνν , and zν /zνν , see Table 6.6. Using (6.251) and (6.252) in combination with GC = 2π(GD)2 and C = 2(zν D)2 (see (6.246) and (6.231)), we can express the variances K(t) in terms of the functions D(t). Finally, by means of the time-dependent solutions of D(t) given by (6.240-6.242) and (6.250), we can compute the evolution of the respective variances: 1 zrσ 1 (1 − exp(−2γt)) = (1 − exp(−2γt)) , (6.253) br zrr 2r br 2 1 z qσ 1+q (1 − q) T K(t) = [zq ] (1 − exp(−[1 + q]γt)) zq b q 2 1 1 1+q (1 − q) , (6.254) [zq ] (1 − exp(−[1 + q]γt)) = 3q − 1 bq

R

K(t) =

272


Table 6.6. Some relations between Gamma-functions and the ratios zνσ /zν , zνσ /zνν , and zν /zνν

9 Γ

ν 1−ν

Γ

9 Γ

Γ

3ν − 1 2(1 − ν)

ν ν−1

Γ

:G 9

H Γ

:G 9

3ν − 1 2(1 − ν)

1 1−ν

Γ

: =

1+ν 2(1 − ν)

2ν − 1 ν−1

H Γ

Γ (x) 1 = Γ (x + 1) x

: =

=

Γ (x) 1 = Γ (x + 1) x

Γ (x) 1 = Γ (x + 1) x

5ν − 3 2(ν − 1)

=

Γ (x) 1 = Γ (x + 1) x

x=

ν (1 − ν)

ν1

x=

3ν − 1 2(ν − 1)

ν>1

zνσ 1 1 3ν − 1 zνσ zν = = = , , zν 3ν − 1 zνν 2ν zνν 2ν

⎡ K(t) = ⎣

G

Q

zrσ SM K(t) = zr

√

ν > 1/3

2 ⎤ (1−q) 1+q 2πe (1 − exp(−[1+q]γt))⎦ , γ

(6.255)

2 Kr,q 1+q (1−q) [zr ] (1 − exp(−[1+s]γt)) br

2 1 Kr,q 1+q (1−q) . = [zr ] (1 − exp(−[1+s]γt)) 3r − 1 br (6.256) Consequently, in the stationary case, we obtain R

Kst =

T

Kst =

1 Q = , 2r br γ 1 3q − 1

6

(1−q) zq

bq

(6.257) 7 2 1+q

,

(6.258)


⎡ Kst = ⎣

G

Q

√

2 (1−q) ⎤ 1+q 2πe ⎦ , γ

273

(6.259)

2 K 1 r,q (1−q) 1+q SM . Kst = [zr ] 3r − 1 br

(6.260)

Diffusion Equations In the case of free Brownian motion, that is, for γ = 0, we are dealing with the nonlinear diffusion equations

−1 2

R r ∂ R ∂ R r P (x, t; u) = Q P dx P , (6.261) ∂x2 ∂t Ω ∂ T ∂ 2 q P (x, t; u) = Q 2 TP , (6.262) ∂t ∂x

⎡ ⎤ ∂ G ⎢ (q−1) P (x, t; u) = Q ⎣e ∂t ∂ SM P (x, t; u) = Q ∂t

P ln GP dx ⎥ ∂ 2 ⎦ 2 ∂x

G Ω

G

P ,

(6.263)

q−r 2

SM r r−1 ∂ SM r P dx P . ∂x2 Ω

(6.264)

These evolution equations are solved again by transient solutions of the form (6.230) and (6.245), because in the preceding discussion we did not exclude the case γ = 0. In order to determine the evolution of the coefficients D(t) we can now proceed in two ways: either we perform the limit γ → 0 in the time-dependent solutions D(t) given by (6.240-6.242) and (6.250), or we solve the corresponding evolution equations (6.237-6.239) and (6.247) under the initial condition u(x) = δ(x − x0 ) putting γ = 0. Both approaches yield the following results: 6 R

D(t) = 6

T

D(t) =

71 1 2

zrr 1 4rQ [zr ]3 t

6 =

71 1 2

1 2

2(3r − 1)Q [zr ]

7 1 1 1+q

1 1 2q(1 + q)Q [zq ]2 t

1 7 6 √ q−1 1 1+q ( e) G , D(t) = 2π(1+q)Q t

,

t

,

(6.265)

(6.266)

(6.267)

274


6 SM

D(t) =

7 1 1 1+q

1 1 2r(1+q)Q Kr,q [zr ]2 t

,

(6.268)

and m(t) = x0 .

(6.269)

The functions C(t) can be derived from C = 2π( D) and for = G from C = 2(zν D)2 (see (6.231) and (6.246)) and read

G

G

2

R

C(t) =

1 1 1 zrr 1 = , 2rQ zr t (3r − 1)Q t

⎤ 2 1 1⎦1 + q 1 T , C(t) = 2 ⎣ 2q(1 + q)Q [z ](1 − q) t q

(6.270)

⎡

⎤ 2 √ (q−1) 1 ⎦ 1+q ( e) G , C(t) = 2π ⎣ 2π(1+q)Q t

(6.271)

⎡

⎤ 2 1 1 ⎦ 1+q 1 SM . C(t) = 2 ⎣ 2r(1+q)Q K [z ](1−q) t r,q r

(6.272)

⎡

(6.273)

The solution (6.230) for (, ν) = (T, q) with TD(t) and TC(t) given by (6.266) and (6.271) corresponds to the Barenblatt–Pattle solution (6.168). Finally, we compute the variances K from (6.251) and (6.252) as R

K(t) = 2Q t ,

(6.274)

2 1 1+q (1 − q) T , 2q(1 + q)Q [zq ] K(t) = t 3q − 1 6 G

K(t) = (1+q)

9√

7 2 :(1−q) 1+q , 2πe Qt

2 1 1+q (1−q) SM . 2r(1+q)Q Kr,q [zr ] K(t) = t 3r − 1

(6.275)

(6.276)

(6.277)

Equations (6.274-6.277) can also be derived directly from (6.253-6.256) by taking the limit γ → 0. We find anomalous diffusion processes in three cases


275

– the entropy Fokker–Planck equations related to the nonextensive entropy functionals TSq , GSq , and SM Sq,r . For r, q > 1 the variances (6.275), (6.276), and (6.277) scale slower than t and, consequently, the corresponding solutions evolve subdiffusively. For r ∈ (1/3, 1) and q ∈ (0, 1) the variances scale faster than t, implying that the corresponding solutions evolve superdiffusively. The solution (6.230) of the Renyi Fokker–Planck equation (6.261) related to the extensive Renyi entropy represents a normal diffusion process, see (6.274). Moreover, the variance of the diffusion process defined by the Renyi FokkerPlanck equation (6.261) evolves exactly like the variance of a Wiener process defined by (3.143). These findings nicely illustrate the general relationship between extensivity and anomalous diffusion addressed in Sect. 6.2.2: entropy Fokker–Planck equations of extensive entropy and information measures describe normal diffusion processes, whereas if we deal with nonextensive entropy and information measures we have anomalous diffusion processes. In this context, it is worth mentioning that (6.274) can also be obtained by substituting the Renyi entropy with G = 0 into the relations (6.37) and (6.38) derived in Sect. 6.2.2. Interpretation of r and q The meaning of the two parameters of the Sharma–Mittal entropy within the framework of entropy Fokker–Planck equations now becomes apparent. We have shown that anomalous diffusion is directly related to the parameter q, which measures the degree of nonextensivity of the entropy SMSq,r . In contrast, the parameter r measures the distortion of the shape of probability densities with respect to the shape of a Gaussian probability density. This distortion can result in cut-off solutions (r > 1), can induce the divergence of variances and the divergence of the entropy functional TSq (r ↓ 1/3, q < r), or leads to variances converging to zero (r ↓ 1/3, q > r). In the special case of the entropy TSq and the corresponding Fokker–Planck equation (6.216), r and q collapse into a single parameter. Consequently, the phenomena of shape-distortion and anomalous versus normal diffusion are intertwined. Figure 6.14 provides a summary of the results obtained so far. The parameter space (r, q) is divided into two regions by the horizontal line q = 1 that represents the one-parametric Renyi entropy RSr . For q > 1 we have subdiffusion and for q ∈ (0, 1) superdiffusion. In addition, we can distinguish two further regions. They are separated by the vertical line r = 1 representing the one-parametric functional GSq . On the right-hand side, that is, for r > 1, there exist stationary cut-off solutions, whereas on the left-hand side, that is, for r ∈ (1/3, 1), we find power law distributions. Note that power law distributions have in particular been studied in the context of the Renyi entropy [28, 39, 389, 636].


normal

diffusion Gaussian

1

0

0 1/3 1 r power law cut-off (γ>0) stationary solutions

superdiffusion

probability densities

subdiffusion

q

transient solutions ( γ = 0 )

276

Fig. 6.14. Key properties of the solutions of the entropy Fokker–Planck equation (6.218) as functions of r and q. The parameter q determines dynamic properties of the transient solutions. There are two separated regions: q > 1 results in subdiffusion; 0 < q < 1 in superdiffusion. The parameter r measures the degree of shape-distortion of the stationary solutions with respect to the Gaussian distribution. There are two separated regions: for r > 1 we have cut-off solutions; for 1/3 < r < 1 we have power c 2000, with permission from Elsevier law distributions; reprinted from [191],

Transition Probability Densities of the Gaussian Entropy Fokker–Planck Equation So far, the focus has been on the evolution of the probability density P (x, t; u). In what follows, we will study the evolution of joint probability densities such as P (x, t; x , t ; u) and P (x, t; x , t ; x , t u) of the entropy Fokker–Planck equation related to the Gaussian entropy (6.208) [181]. To this end, we write (6.217) as ∂ ∂ ∂ P (x, t; u) = γxP + Q exp{(1 − q) BS[P ]} 2 P . ∂t ∂x ∂x

(6.278)

Note that in this paragraph we will drop in most cases the upper index G. Equation (6.278) involves the diffusion coefficient D2 (P ) = Q exp{(1 − q) BS[P ]}. If for a solution P (x, t; u) the coefficient D2 (x, t, u) = D2 (P ) corresponds to the second Kramers–Moyal coefficient of a Markov diffusion process, then this Markov process is described by the solution P (x, t; u) and the transition probability density P (x, t|x , t ; u) defined by (see Sect. 3.2) ∂ P (x, t|x , t ; u) = ∂t


277

∂ ∂ γxP (x, t|x , t ; u) + Q exp{(1 − q) BS[P (x, t; u)]} 2 P (x, t|x , t ; u) , ∂x ∂x (6.279) Therefore, let us consider the exact transient solution derived above, which reads [x − M1 (t)]2 1 (6.280) exp − P (x, t; δ(x − x0 )) = 2K(t) 2πK(t) and involves the first moment M1 (t), M1 (t) = x0 exp{−γ(t − t0 )} ,

(6.281)

and the variance K(t), K(t) =

2/(1+q) Q [2πe](1−q)/2 (1 − exp{−(1 + q)γ(t − t0 )}) γ

(6.282)

and converges in the long time limit to 0 1 x2 Pst (x) = , exp − 2πKst 2Kst with

Q [2πe](1−q)/2 Kst = γ

(6.283)

2/(1+q) .

(6.284)

From (6.224) it follows that for the transient solution (6.280) the diffusion coefficient reads D2 (t, δ(x − x0 )) = D2 (P ) = Q/ G U(t). Let us collect (6.246), (6.248), and (6.251): G

C(t) = 2

!√

"2 π D(t) , G

G

1−q G D(t) √ , U(t) = e

G

K(t) =

1 . C(t) (6.285)

G

Then, we obtain D2 (t, δ(x − x0 )) = D2 (P ) = Q/ G U(t) = [2πeK(t)](1−q)/2

(6.286)

and we see that D2 can indeed be regarded as the second Kramers–Moyal coefficient of a Markov diffusion process. Consequently, for the transient solution (6.280) the Gaussian entropy Fokker–Planck equation (6.279) reads ∂ ∂ ∂ P (x, t|x , t ; δ(x − x0 )) = γxP + Q[2πeK(t)](1−q)/2 2 P ∂t ∂x ∂x

(6.287)

and defines the transition probability density of a Markov diffusion process. Equation (6.287) is solved by

278


P (x, t|x , t ; δ(x − x0 )) =

1 [x − M1 (t, t )]2 , exp − 2πK(t, t ) 2K(t, t )

(6.288)

where M1 (t, t ) and K(t, t ) describe the first moment and variance with re(1+q)/2 spect to x. Substituting (6.288) and Q[2πe](1−q)/2 /γ = Kst (see (6.284)) into (6.287), we obtain M1 (t, t ) = x exp{−γ(t − t )}

(6.289)

and

9 : ∂ (1+q)/2 (1−q)/2 K(t, t ) = −2γ K(t, t ) − Kst K (t) . (6.290) ∂t Solving (6.290) for the initial condition limt→t K(t, t ) = 0, we obtain K(t, t ) = 2γKst

(1+q)/2

t

t

exp{−2γ(t − z)}[K(z)](1−q)/2 dz .

(6.291)

Equations (6.280), (6.281), (6.282), (6.288), (6.289), and (6.291) provide us with a complete description of the generalized Ornstein–Uhlenbeck process related to the nonextensive entropy measure GSq in terms of the expressions P (x, t; δ(x−x0 )) and P (x, t|x , t ; δ(x−x0 )) and M1 (t), K(t), M1 (t, t ), K(t, t ). Let us discuss the approach to the stationary case and some numerical issues. Let us consider the stationary case in terms of the limit t → ∞ (which implies t → ∞ because of t ≥ t ). Then, K(z) in (6.291) converges to Kst and, consequently, (6.291) becomes lim K(t, t ) = Kst (t − t ) = Kst [1 − exp{−2γ(t − t )}] ,

t →∞

(6.292)

which means that the transition probability density (6.288) becomes stationary: (6.293) lim P (x, t|x , t ; δ(x − x0 )) = Pst (x, t − t |x ) . t →∞

In order to discuss the asymptotic behavior in this stationary case, we consider the limiting case given by t → ∞ and t − t → ∞. Then, we have M1 (t, t ) = 0 and K(t, t ) = Kst , which implies that lim

t−t →∞,t →∞

P (x, t|x , t ; δ(x − x0 )) =

lim

t−t →∞

Pst (x, t − t |x ) = Pst (x) . (6.294)

The Ito–Langevin equation of (6.279) reads (see Sect. 3.4) d X(t) = −γX(t) + Q exp{(1 − q) BS[P ]} Γ (t) . dt

(6.295)

In order to solve (6.295), we will use the averaging method of self-consistent Langevin equations, see Sect. 3.4.4. Let us show in detail how this method


1.5

279

K(t)

1 0.5

K(t,t’) 0.5

1

1.5

2.5

2

0

t

–0.5 –1 –1.5

M1(t)

–2

Fig. 6.15. M1 (t), K(t), and K(t, t ) for q = 1.3. For t ≤ t we have put K(t, t ) = 0. Parameters: γ = 0.5, x0 = −2, t0 = 0, Q = 1, t = 0.7, x = −1. (L = 5000, ∆t = 0.01, 2[∆x]2 = 0.1, wn via Box–Muller)

4

K(t)

3 K(t,t’)

2 1 0

0.5

–2

1

1.5

2

3

2.5 t

–1 M1(t)

Fig. 6.16. M1 (t), K(t), and K(t, t ) for q = 0.7 and L = 20000; other parameters as in Fig. 6.15

works for (6.295). First, we interpret (6.295) as the Langevin equation of anonlinear family of Markov diffusion processes, dX(t)/dt = −γX(t) + D2 (t) Γ (t), and use the Euler forward scheme X l (tn + ∆t) = X l (tn ) − ∆tγX l (tn ) + Q∆t exp{(1 − q) BS[P ]} wnl (6.296) to compute the realizations X l of X. Accordingly, the random variable X(t) is evaluated at times tn = n∆t for n = 0, 1, 2, . . .. The variables wnl are realizations of Gaussian distributed random variables wn satisfying wn = 0 and wi wk = 2δik , see Sect. 3.4.4. Next, we use (3.49), that is, δ(x −

280


√ x0 ) = exp{−(x − x0 )2 /(2[∆x]2 )}/[ 2π∆x] for ∆x → 0, and P (x, t; u) = δ(x − X(t)) and write 2 L 1 1 x − X l (t) P (x, t; u) = √ (6.297) exp − 2 ∆x L 2π∆x l=1

for ∆x small and L large. Then, from BS[P ] = − ln P it follows that 6 2 7 L L 1 1 1 X k (t) − X l (t) B √ . (6.298) S[P ] = − ln exp − L 2 ∆x L 2π∆x l=1 k=1 In sum, (6.296) becomes X l (tn + ∆t) = X l (tn ) − ∆tγX l (tn ) # 6 $ 7 L L $ (q−1) 1 [X k (tn )−X l (tn )]2 l% √ +wn Q∆t exp ln exp − L 2[∆x]2 L 2π∆x l=1 k=1

.

(6.299) In Figs. 6.15 and 6.16 we have plotted M1 (t), K(t) and K(t, t ) for q > 1 and q < 1, respectively. We have computed these quantities both from the analytical expressions (6.281), (6.282), and (6.291) (solid lines) and from the Langevin equation (6.295) by solving (6.299) iteratively (diamonds). Note that in order to derive K(t, t ) we evaluated only a small subset of all simulated trajectories, namely, the trajectories X l (t) that assume at time t = t the value x . The reason for this is that K(t, t ) is the variance of X(t) given that the condition X(t ) = x is satisfied. For further simulations involving other q-parameters see [181]. 6.5.4 Fokker–Planck Equations for Fermions and Bosons In order to account for the the quantum statistics of particles, we will consider now free energy Fokker–Planck equations with free energies that involve quantum mechanical entropies. In doing so, we will obtain nonlinear Fokker–Planck equations that describe statistical properties of many-body systems composed of quantum particles. Moreover, nonlinear Fokker–Planck equations of this kind can describe the evolution of distribution functions of quantum particles. Drift- and Diffusion Forms Let ρ(x) denote the mean occupation number density of Fermi or Bose particles that live in a continuous phase space Ω. Then, we may describe the free energy of the quantum mechanical many-body system by means of


F [ρ] = UL [ρ] − T

FD,BE

S[ρ] ,

281

(6.300)

where the quantum mechanical entropy FD,BES is given by (6.107) and UL = U (x)ρ(x) dx. Substituting (6.300) into the univariate version of (4.62), Ω 0 we obtain the evolution equation ∂ ∂ dU0 (x) ∂ ρ(x, t) ∓ T ln {1 ∓ ρ(x, t)} , (6.301) ρ(x, t) = M (ρ) dx ∂x ∂t ∂x where M (ρ) denotes a density-dependent mobility coefficient. For M = 1 we get ∂ ∂ dU0 (x) ∂2 ρ(x, t) = ρ(x, t) ∓ T 2 ln {1 ∓ ρ(x, t)} . ∂t ∂x dx ∂x

(6.302)

Equation (6.302) has been proposed as a classical stochastic description of fermions and bosons [165, 190, 193, 192, 323]. The upper sign is related to Fermi systems, the lower sign to Bose systems. Equation (6.302) can be regarded as the diffusion form of the entropy Fokker–Planck equation (6.301). In order to obtain the corresponding drift form, we first note that from (6.302) ˆ s (ρ) = ± ln[1 ± ρ] holds. Next we note that we conclude that the relation L FD,BE for S the mobility coefficient (6.48) reads 6 7−1 ˆ s (ρ) dL M (ρ) = =1∓ρ . (6.303) dρ Substituting this expression into (6.301), we obtain ∂ dU0 (x) ∂ ∂2 ρ(x, t) = (6.304) [1 ∓ ρ(x, t)]ρ(x, t) + T 2 ρ(x, t) . ∂t ∂x dx ∂x As suggested by Kaniadakis and Quarati the drift form and its multivariate generalization can be derived using exclusion and inclusion principles related to Fermi and Bose statistics [327, 328]. Alternatively, the drift form (6.304) can also be derived using heuristic arguments [318]. In general, nonlinear Fokker-Planck equations for quantum particles can be derived from quantum mechanical Boltzmann equations [53, 154, 596] taking the so-called kinetical interaction principle into account [322, 323]. Stationary Solutions Stationary distributions of (6.302) and (6.304) that obey the free energy principle δF/δρst = µ can be derived from (6.108) and read ρst (x) =

1 , exp{ [U0 (x) − µ]/ T } ± 1

(6.305)

see also Sect. 6.4.2. Equation (6.305) describes quantum mechanical distributions of particles or subsystems that behave like fermions (upper sign) or bosons (lower sign).

282


Approach to Stationary Solutions Since the quantum mechanical entropy measures FDS and BES are strictly concave, the corresponding free energy measures are bounded from below and the H-theorem of free energy Fokker–Planck equations applies, which implies that we have limt→∞ ∂ρ/∂t = 0. This approach of transient solutions to stationary ones has also been illustrated by means of numerical studies [377]. Langevin Equations and Autocorrelations Using P (x, t; u) = ρ(x, t)/M0 , we can transform (6.302) and (6.304) into T ∂2 ∂ ∂ dU0 (x) ∓ (6.306) ln {1 ∓ M0 P } , P (x, t; u) = P ∂t ∂x dx M0 ∂x2 ∂ dU0 (x) ∂2 ∂ P (x, t; u) = [1 ∓ M0 P ]P + T 2 P . (6.307) ∂t ∂x dx ∂z For the Fermi systems we require that P < 1/M0 (which corresponds to the requirement ρ < 1). Note that (6.307) and (6.306) correspond to the entropy Fokker–Planck equations (6.46) and (6.50) involving the entropy

1 FD,BE [1 ∓ M0 P (x)] ln[1 ∓ M0 P (x)] dx . S[P ] = − P (x) ln P (x) dx ∓ M0 Ω (6.308) Stationary distributions now read 1 Pst (x) = . (6.309) M0 [exp{ [U0 (x) − µ]/ T } ∓ 1] Equation (6.306) can be written in the form of a general nonlinear Fokker– Planck equation (2.10) with D2 (P ) = ∓T M0−1 ln(1 ∓ P )/P , which is not defined for P = 0 but is well-defined in the limit P → 0 because of limz↓0 ∓T M0−1 ln(1 ∓ z)/z = limz↓0 ±T M0−1 1/(1 ∓ z) = 1 (rule of de l‘Hopital). Furthermore, we have D2 (P ) > 0 for P > 0 (and P < 1/M0 in the Fermi case). Consequently, for initial distributions u(x), for which (6.306) yields positive-definite C ∞ -solutions P (x, t; u), we can regard D2 (x, t; u) = D2 (P ) = ∓T M0−1 ln(1 ∓ P )/P as the time and space-dependent second order Kramers–Moyal coefficient of a linear Fokker–Planck equation, which implies that (6.306) can be regarded as a strongly nonlinear Fokker–Planck equation. A complete description of the stochastic processes described by (6.306) can then be obtained from the solutions P (x, t; u) and the transition probability density P (x, t|x , t ; u) defined by ∂ dU0 (x) ∂ P (x, t|x , t ; u) = P (x, t|x , t ; u) ∂t ∂x dx ∂ 2 ln {1 ∓ M0 P (x, t; u)} ∓T 2 P (x, t|x , t ; u) . ∂x M0 P (x, t; u) (6.310)


283

The Ito–Langevin equation corresponding to (6.306) and (6.310) reads √ d X(t) = h(X) + T ζ(X(t), t) , dt

with ζ(y, t) =

± ln {1 ± M0 P (y, t; u)} Γ (t) M0 P (y, t; u)

(6.311)

(6.312)

and h(x) given by h(x) = −dU0 (x)/dx. Here, ζ(X, t) can be considered as a probability-dependent multiplicative fluctuating force. Likewise, for classical solutions P (x, t; u) of (6.307) we can interpret the expression D1 (x, t; u) = D1 (x, P ) = −dU0 (x)/dx)[1 + M0 P ] as a time and space-dependent drift term of a linear Fokker–Planck equations, which means that (6.307) becomes a strongly nonlinear Fokker–Planck equation. In this case, the stochastic processes of interest can be computed from P (x, t; u) defined by (6.307) and P (x, t|x , t ; u) described by ∂ ∂ dU0 (x) P (x, t|x , t ; u) = [1 ∓ M0 P (x, t; u)]P (x, t|x , t ; u) ∂t ∂x dx ∂2 (6.313) +T 2 P (x, t|x , t ; u) . ∂x Alternatively, P (x, t; u) and P (x, t|x , t ; u) can be obtained from √ d X(t) = h(X) [1 ± M0 P (x, t; u)]|x=X(t) + T Γ (t) , dt

(6.314)

for h(x) = −dU0 (x)/dx. In sum, both from the drift and diffusion forms the joint probability densities P (x, t; x , t ; u) = P (x, t|x , t ; u)P (x , t ; u), P (x, t; x , t ; x , t ; u) = P (x, t|x , t ; u)P (x , t |x , t ; u)P (x , t ; u) and so on can be derived. From these joint distributions, in turn, we obtain the density measures ρ(x, t; x , t ) = M0 P (x, t; x , t ; u) = P (x, t|x , t ; u)ρ(x , t ) , ρ(x, t; x , t ; x , t ) = M0 P (x, t; x , t ; x , t ; u) = P (x, t|x , t ; u)P (x , t |x , t ; u)ρ(x , t ) ... ,

(6.315)

see also (3.23). These density functions provide us with the information about all possible autocorrelation functions of systems described by the quantum mechanical Fokker–Planck equations (6.302) and (6.304). Nonlinearities and Distributions Let us dwell on the drift form of the Fermi and Bose Fokker–Planck equation (6.307). For (6.307) related to the Bose statistics we may introduce the effective force D1 (x, P ) = h(x)[1 + M0 P ]. We see that the force h(x) is weighted

284


by an expression involving the probability density in such a way that at positions where the probability density is large, the amount of h(x) is increased. In consequence, if h(x) is attractive at a particular position x∗ , the probability density is increased at x∗ and, in turn, the amount of the effective force heff (x∗ ) is increased. Thus, the stationary probability densities of (6.307) in the case of the plus sign are more pronounced at the attractive points of h(x) than those of the corresponding linear Fokker–Planck equations. This conclusion is in accordance with the notion that bosons have the tendency to gather to a greater extent at the states of minimal energy than particles described by the Maxwell–Boltzmann statistics. Furthermore, as far as (6.307) for fermions is concerned, we may infer by analogy that the stationary probability density is less pronounced at the attractive points of the force h in comparison with the stationary probability density of the corresponding linear Fokker–Planck equation – an inference that is in agreement with the fact that fermions repulse each other and avoid aggregation at a particular state. Interpretation of the Univariate Case: Overdamped Motion We may interpret the univariate equations as descriptions for the overdamped motion of fermions and bosons, where x is the position of the particles (Smoluchowski limit). Alternatively, we may consider x as the particle velocity of fermions and bosons: x → v. Then, for the parabolic potential U0 (v) = γv 2 /2 with γ > 0 we would deal with particles that are subjected to a linear damping force: h(v) = −γv. 6.5.5 Multivariate Generalizations We discuss here three multivariate entropy Fokker–Planck equations that may be of particular interest [193]. They correspond to special cases of the Kramers equation (4.107) for vanishing mean field terms. Generalized Kramers Equation for Linear Internal Energy Functionals For HMF = 0 the evolution equation (4.107) reduces to 3 pj ∂ dV (q) ∂ γ ∂ P (p, q, t) − + pj P (p, q, t) = − ∂t m ∂qj ∂pj dqj m j=1 +γQ

dB dz Ω

3 ∂2 ˆ 2 Ls [P (p, q, t)] . (6.316) 3 3 s[P ] d p d q j=1 ∂pj

There might be solutions of (6.316) for which the corresponding Fokker– Planck equation for P (p, q, t|p , q , t ) yields well-defined Markov transition


285

probability densities. These solutions of (6.316) can alternatively be computed from the Ito–Langevin equation pj d qj (t) = , dt m

# $ $ d γ d dB % V (q) + γQ pj (t) = − pj − dt m dqj dz

3

Ω

3

s[P ] d p d q

ˆ s [P ] L Γj (t) , P (6.317)

for j = 1, 2, 3. Kramers Equations for Classical Fermions and Bosons Next, we consider ensembles of fermions and bosons. The multivariate counterparts of the quantum mechanical entropies (6.308) read

(1 − M0 P ) BE S=− P ln P + ln(1 − M0 P ) d3 pi d3 qi , (6.318) M0

(1 + M0 P ) FD S=− P ln P − ln(1 + M0 P ) d3 pi d3 qi (6.319) M0 for the Bose–Einstein statistics and the Fermi–Dirac statistics, respectively. Substituting these entropies with Q = T into (6.316), we obtain 3 pj ∂ dV (q) ∂ γ ∂ P (p, q, t) = − P (p, q, t) − + pj ∂t m ∂qj ∂pj dqj m j=1 ∓

3 γT ∂ 2 ln {1 ∓ M0 P (p, q, t)} , M0 j=1 ∂p2j

(6.320)

where the upper sign holds for fermions and the lower sign for bosons. One can also show that the drift form of the multivariate fermions and bosons Fokker–Planck equations is given by [165, 318, 321, 327, 328] 3 ∂ pj ∂ dV ∂ γ P (p, q, t) = − − + pj [1 ∓ M0 P (p, q, t)] P (p, q, t) ∂t m ∂qj ∂pj dqj m j=1 +γT

3 ∂2 P (p, q, t) . ∂p2j j=1

(6.321)

Again, the upper sign refers to particles with Fermi–Dirac statistics, while the lower sign refers to particles with Bose–Einstein statistics. Stationary

286


solutions of (6.320) and (6.321) describe statistics similar to the Fermi–Dirac and the Einstein-Bose statistics: Pst (p, q) =

1 . 2 p /(2m) + V (q) − µ ±1 M0 exp T

(6.322)

If we consider solutions P (p, q, t) of (6.320) for which (6.320) is a strongly nonlinear Fokker–Planck equation, Markov diffusion processes can be defined by means of the transient solutions P (p, q, t) of (6.320) and the transition probability densities P (p, q, t|p , q , t ) satisfying ∂ P (p, q, t|p , q , t ) = ∂t 3 pj ∂ dV (q) ∂ γ P (p, q, t|p , q , t ) − + pj − m ∂q ∂p dq m j j j j=1 ±γT

3 ∂ 2 ln {1 ± M0 P (p, q, t)} P (p, q, t|p , q , t ) . 2 ∂p M P (p, q, t) 0 j j=1

(6.323)

Then, the stochastic trajectories of fermions and bosons can be computed from the Ito–Langevin equation d pj qj (t) = , dt m

d γ d pj (t) = − pj − V (q) + dt m dqj

±γT

ln {1 ± M0 P (p, q, t)} Γj (t) , M0 P (p, q, t) (6.324)

for j = 1, 2, 3. Likewise, if (6.321) can be regarded as a strongly nonlinear Fokker–Planck equation, Markov diffusion processes can be defined by means of the transient solutions P (p, q, t) of (6.321) and the transition probabilities given by ∂ P (p, q, t|p , q , t ) = ∂t 3 pj ∂ dV ∂ γ − + pj [1 ± M0 P (p, q, t)] P (p, q, t|p , q , t ) − m ∂q ∂p dq m j j j j=1 +γQ

3 ∂2 2 P (p, q, t|p , q , t ) . ∂p j j=1

(6.325)

Alternatively, the processes can be obtained from the Langevin equation


287

pj d qj (t) = [1 ± M0 P (p, q, t)] , dt m d d γ pj (t) = − pj + V (q) [1 ± M0 P (p, q, t)] + γT Γj (t) . dt m dqj (6.326) The density functions ρ(p, q, t), ρ(p, q, t; p , q , t ),. . . can be derived by means of ρ(p, q, t) = M0 P (p, q, t) , ρ(p, q, t; p , q , t ) = M0 P (p, q, t; p , q , t )P (p , q , t ) ...

(6.327)

Alternatively, they may be computed from the stochastic trajectories X(t) = (p(t), q(t)): ρ(p, q, t) = M0 δ(p − p(t)) δ(q − q(t)) , ρ(p, q, t; p , q , t ) = M0 δ(p − p(t)) δ(q − q(t)) δ(p − p(t )) δ(q − q(t )) ... (6.328) Quantum mechanical energy distributions Finally, we may defined stochastic paths of quantum particles in energy space by means of the Kramers equations (6.320) and (6.321) and the Langevin equations (6.324) and (6.326), respectively. In order to illustrate the main point here, let us consider a spatially homogenous and isotropic system with V (q) = 0. In this case the energy (t) of a particle is given by the kinetical energy (t) = p2 (t)/[2m]. First, we note that realization of (t) can be computed from the Langevin equations (6.324) and (6.326) if we solve them numerically for p(t) and subsequently put (t) = p2 (t)/[2m]. The energy distribution can then be obtained from the realizations of (t) like P (, t) = δ( − (t)) .

(6.329)

Alternatively, we introduce the distribution P (p, t) of the magnitude of the momentum p = |p|: P (p, t) = δ(p − p(t)). Since in the isotropic system the probability to find a particle with p < |p| < p + dp is given by 4πP (p, t)p2 dp, on the one hand, and P (p, t)dp, on the other, we obtain (6.330) P (p, t) = 4πp2 P (p, t)|p|=p . The distribution of particle energies P (, t) satisfies P (, t)d = P (p, t)dp [498]. Using d = 2m−1 p dp and (6.330), we get P (, t) = 2πmpP (p, t) and √ P (, t) = [2m]3/2 π P (p, t) . (6.331) |p|2 /[2m]=

288


That is, the energy distributions P (, t) can be obtained from the isotropic solutions P (p, t) of the aforementioned Kramers equation and the Langevin equations for quantum particles. For example, in the stationary case from (6.322) and (6.331) with V (q) = 0 we obtain √ a , (6.332) Pst () = −µ ±1 exp T with a = [2m]3/2 πM0−1 . In fact, Pst () describes the energy distribution of Fermi and Bose systems that are composed of particles with finite mass m, √ where the factor corresponds to the density of quantum states. We will return the issue of quantum energy distributions in Sect. 6.5.6 and present there an alternative approach. Kramers Equations for the Entropy by Tsallis Substituting the entropy functional TSq given by (6.121) into (6.316), we obtain 3 3 ∂ pj ∂ dV ∂2 q ∂ γ P (p, q, t) = − P + γQ − + pj P . m ∂qj ∂pj dqj m ∂p2j ∂t j=1 j=1 (6.333) For q ∈ (0, 1) stationary probability densities can be derived from (4.108) and are found as 1/(q−1) ! 2 " p /(2m) + V (q) 1 1−q + −µ . Pst (p, q) = q 1−q Q (6.334) Note that for q = 1 the generalized Kramers equation (6.333) recovers the classical Kramers equation. Similarly, in the limit q → 1 the stationary solution (6.334) reduces to a Boltzmann distribution of the Hamiltonian p2 /(2m) + V . For q > 1 we are dealing with cut-off distributions, which usually require more detailed analysis. Multivariate nonlinear Fokker–Planck equations similar to (6.333) have been studied by Compte et al. [99, 100] and Borland et al. [68]. Equation (6.333) can be considered as a possible modification of the univariate entropy Fokker–Planck equation proposed by Plastino and Plastino that has been discussed in Sect. 6.5.2. 6.5.6 Metal Electron Model, Black Body Radiation Model, and Planck’s Radiation Formula In Sects. 6.5.4 and 6.5.5 we have considered quantum mechanical many-body systems in phase spaces spanned by a one-dimensional coordinate x and by


289

momentum and position vectors p and q. In this section, we extend the scope of our previous considerations in order to describe the evolution of quantum systems in the energy phase space. In doing so, we will be able to derive nonlinear Fokker–Planck equations for stochastic processes that are consistent with the experimentally observed energy distributions of electrons in metals and photons in black body cavities. Let gi > 0 describe the number of different quantum states that belong to the same energy level i , that is, the degeneration of the energy level i . Then the quantum entropy (6.98) becomes [14, 302, 373] S(ρ1 , . . . , ρN ) = −

FD,BE

N

ρi ln ρi +

N

gi ln gi ∓

i=1

i=1

N

(gi ∓ ρi ) ln(gi ∓ ρi ) .

i=1

(6.335) Note that here and in what follows the upper sign refers to Fermi systems, while the lower sign refers to Bose systems. In the special case of a vanishing degeneration (i.e., for gi = 1) the entropy (6.335) recovers the entropy measure (6.98) of the nondegenerated case. In the case of Fermi systems we require that ρi < gi for temperatures T > 0. For T = 0 we have ρi = gi up to the Fermi energy F and ρi = 0 for energy states i with i > F . Studying systems with continuous energy levels ∈ Ω = [0, ∞), we replace gi by a function g() ≥ 0. The expression g() d describes the number of states in an energy range between and + d. That is, g() describes the density of states with respect to the energy scale [14, 410, 490, 619]. Using g(), we may modify (6.99) in order to obtain

FD,BE g() ln g() d ρ() ln ρ() d + S[ρ] = − Ω

Ω [g() ∓ ρ()] ln[g() ∓ ρ()] d . (6.336) ∓ Ω

In the case of Fermi systems the constraint ρ() < g() for T > 0 holds. Now, let us consider the free energy F [ρ] = U [ρ] − T

FD,BE

S[ρ]

(6.337)

with U [ρ] =

ρ() d .

(6.338)

Ω

In order to derive stationary distributions ρst from the free energy principle δF/δρ = µ, we need to compute the variational derivatives of U and FD,BES. They read δU = (6.339) δρ and

290


δ FD,BE S = − ln δρ

ρ g∓ρ

.

(6.340)

From δF/δρ = µ and by means of (6.337), (6.339), and (6.340), we obtain the Fermi–Dirac and Bose–Einstein distributions for quantum systems with degenerated energy levels: ρst () =

g() . exp{( − µ)/T } ± 1

(6.341)

The free energy Fokker–Planck equation for the density ρ(, t) can be obtained from (4.13) by replacing x with . Thus, we get ∂ ∂ ∂ δF . ρ(, t) = ρ ∂ ∂ δρ ∂t

(6.342)

Using (6.337), (6.339), and (6.340), we obtain ∂ ∂ρ ∂ ∂ ρ ρ(, t) = +T ρ . ∂t ∂ ∂ ∂ g ∓ ρ

(6.343)

Y

Let us evaluate the expression Y . A detailed calculation shows that ρ

dg ∂ ρ d = ± [1 + ln(g ∓ ρ)] ∓ [g ln(g ∓ ρ)] . d d ∂ g ∓ ρ

With this result at hand, (6.343) can be written as ∂ρ ∂ dg ∂2 ∂ ρ(, t) = ±T [1 + ln(g ∓ ρ)] ∓ T 2 g ln(g ∓ ρ) . ∂t ∂ ∂ d ∂

(6.344)

(6.345)

Equation (6.345) is well-defined in the limit ρ → 0 because (6.345) is homogenous with respect to ρ. That is, ρ = 0 is a solution of (6.345) (which can be verified by substituting ρ = 0 into (6.345)). In order to obtain a semipositive definite diffusion coefficient, we write the term g ln(g ∓ ρ) in (6.345) as g ln(g ∓ ρ) = g ln(1 ∓ ρ/g) + g ln(g), which gives us T dg ∂2 ∂ ρ ρ ∂ ρ(, t) = − ln 1 ∓ −1 ∓ ρ ∓ T 2 g ln 1 ∓ . ∂t ∂ ρ d g ∂ g (6.346) Note that we have a reflective boundary at = 0 with ρ(0, t) = 0. Furthermore, we will consider only functions g() with g(0) = 0. In view of the term ln(1 ∓ ρ/g) occurring in (6.346), we restrict our considerations to solutions ρ(, t) of (6.346) for which in the limit → 0 the ratio ρ/g is finite for all t ≥ t0 . The drift and diffusion coefficients read T dg() ρ , (6.347) d1 (, ρ) = −1 ∓ ln 1 ∓ ρ d g() ρ g() d2 (, ρ) = ∓T ln 1 ∓ . (6.348) ρ g()


291

The diffusion coefficient d2 is positive definite, which can be seen if we distinguish explictly between Fermi and Bose systems. For Fermi systems we obtain d2 = T g ln(1/(1 − ρ/g)) > 0 for 0 < ρ() < g(). For Bose systems we have d2 = T g ln(1 + ρ/g)) > 0 for ρ() > 0. By similar reasonings, we see that the drift term is composed of an attractive and repulsive part: d1 = d1 (−)+d1 (+). The attractive part is given by d1 (−) = −1 and drives the particles to states of zero energy. The repulsive part reads d1 (+) = ∓T ρ−1 dg/d ln(1 ∓ ρ/g) > 0 and drives the quantum particles away from the ground state energy provided that the density of energy states increases with the energy (i.e., we have dg/d > 0). Due to the interplay of these two forces, stable stationary distributions can be established. In the limit ρ/g → 0 the drift and diffusion coefficients become independent of ρ: lim d1 (, ρ) = −1 + T

ρ/g→0

d ln g() , d

lim d2 (, ρ) = T .

(6.349) (6.350)

ρ/g→0

If the occupation number density ρ is normalized to M0 with M0 = Ω ρ() d, we can substitute P (, t; u) = ρ(, t)/M0 into (6.346) and thus obtain a nonlinear Fokker–Planck equation for the probability density P . We proceed now under the hypothesis that the Fokker–Planck equation thus obtained is a strongly nonlinear Fokker–Planck equation. Then, the transition probability density P (, t| , t ; u) of the stochastic process related to (6.346) satisfies P (, t| , t ; u) =

∂ ∂2 d1 (, ρ(, t))P + 2 d2 (, ρ(, t))P , ∂ ∂

(6.351)

with u() = ρ(, t0 ), and higher order density distributions can be obtained from ρ(, t; , t ) = P (, t| , t ; u)ρ( , t ) , ρ(, t; , t ; , t ) = P (, t| , t ; u)P ( , t | , t ; u)ρ( , t ) ··· ,

(6.352)

see also Sect. 3.2. Alternatively, higher order density functions can be computed from the ensemble averages ρ(, t; , t ) = M0 δ( − L (t))δ( − L (t )) , ρ(, t; , t , , t ) = M0 δ( − L (t))δ( − L (t ))δ( − L (t )) ··· ,

(6.353)

where L (t) is given by the two-layered Ito–Langevin equation (see Sect. 3.4.1) d L (t) = d1 (L , ρ(L , t)) + d2 (L , ρ(L , t))Γ (t) dt

(6.354)

292


and ρ(, t) is a solution of (6.346). Both ρ(, t) = M0 δ( − L (t)) and higher order density functions (6.353) can be computed from the self-consistent Ito– Langevin equation (see Sect. 3.4.2) dg() d M0 δ( − L (t)) T L (t) = −1 ∓ ln 1 ∓ dt M0 δ( − L (t)) d g()

= L (t) M0 δ( − L (t)) g() ln 1 ∓ + ∓T Γ (t) , (6.355) g() M0 δ( − L (t))

= L (t)

see Sect. 3.4.2. Let us apply now the Ito–Langevin equation (6.355) to describe the quantum statistics of electron gases and black body radiation. Metal Electron Model The electrons of the conduction band of metals can be regarded as a gas of fermions distributed over a continuous energy scale. In what follows we consider a free electron gas for which contributions of the potential energy to the total energy of the gas can be neglected. For the free electron gas √ the density of states is given by g() = a with a > 0 [14, 410, √ 490, 619]. Consequently, for the free electron gas we have dg/d = a/(2 ) and the Fermi Fokker–Planck equation (6.346) (upper sign) becomes ρ aT ∂ ∂ −1 − √ ln 1 − √ ρ ρ(, t) = − ∂t ∂ 2 ρ a ∂2 √ ρ −aT 2 ln 1 − √ . (6.356) ∂ a The corresponding Ito–Langevin equation (6.355) reads d M0 δ( − L (t)) aT √ √ ln 1 − L (t) = −1 − dt 2M0 δ( − L (t)) a

= L (t) √ M0 δ( − L (t)) a √ ln 1 − + −T Γ (t) . (6.357) M0 δ( − L (t)) a

= L (t)

√ Equation (6.357) is subjected to the constraint ρ() < a for T > 0. From (6.349) and (6.350) we read off that the limiting cases lim d1 (, ρ) = −1 +

ρ/g→0

lim d2 (, ρ) = T

ρ/g→0

T , 2

(6.358) (6.359)


293

0.14 ρ(ε)

0.12 0.1 0.08 0.06 0.04 0.02 0

2

4

ε

6

8

10

Fig. 6.17. Stationary solution of the Fermi Fokker–Planck equation (6.356). Solid line: analytical result (6.360). Diamonds: numerical results obtained by solving (6.357) using the averaging method for self-consistent Ito–Langevin equations. Dashed line: stationary solution in the limiting case T → 0. Parameters: µ = F = 2, T = 1.0, a = 0.1 (L = 5000, ∆t = 0.1, 2[∆x]2 = 0.1, wn via Box–Muller). In order to use a moderately small single time step ∆t, a reflective boundary at b = 0.1 was used. In order to simulate a reflective boundary in the limit b → 0, one needs to use a single time step ∆t → 0 such that ∆t × d1 with d1 given by (6.358) yields not too large values for = b [180]

0.08 ρ(ε) 0.06 0.04 0.02 0

2

4

ε

6

8

10

Fig. 6.18. Stationary solution as in Fig. 6.17 (solid line and diamonds). In addition, the initial distribution used to solve the Ito–Langevin equation numerically is shown. The initial distribution corresponds approximately to a uniform distribution in the range between = 1 and = 4 and satisfies the constraint ρ() < g() [180]

294


hold. In the case of the free electron gas, the stationary solution (6.341) reads √ a , (6.360) ρst () = exp{( − µ)/T } + 1 for T > 0, where µ is referred to as the Fermi energy F . In the limit T → 0 we obtain √ a for ≤ µ = F ρst () = . (6.361) 0 for > µ = F In order to simulate the electron gas by means of the Ito–Langevin equation (6.357)for a particular Fermi energy F , we first compute M0 by means of M0 = Ω ρst () d and substitute the result into (6.357). Figure 6.17 shows the stationary distribution of the free electron gas as obtained from (6.360) and from a simulation of the Ito–Langevin equation (6.357). The dashed line describes the Fermi distribution at T = 0. In order to solve the Ito–Langevin equation (6.357) numerically it is important√to choose an initial distribution that satisfies the constraint ρ() < g() = a , see Fig. 6.18. Black Body Radiation Model and Planck’s Radiation Formula The electromagnetic radiation in a cavity with walls that have a particular temperature T exhibits a frequency distribution ρ(ν) given by Bose–Einstein statistics. The notion is that the radiation field consists of photons. A photon is a Bose particle that describes an electromagnetic wave with a frequency ν and energy = hν, where h is Planck’s constant [14, 269, 490]. We say the black body container is filled up with a photon gas. The density of states of the photon gas is given by g(ν) = aν 2 with a > 0, which implies dg/dν = 2aν. For the sake of conveniency, we put h = 1 such that = ν. Then, the Bose Fokker–Planck equation (6.346) (lower sign) for the photon gas is given by ∂ 2aT ν 9 ∂ ρ : ∂2 2 9 ρ : ρ(ν, t) = − ln 1 + −1 + ρ + aT . ν ln 1 + ∂t ∂ν ρ a ν2 ∂ν 2 a ν2 (6.362) and the Ito–Langevin equation (6.355) reads d M0 δ(ν − νL (t)) 2aT ν νL (t) = −1 + ln 1 + dt M0 δ(ν − νL (t)) aν 2 ν=νL (t) 2 aν T M0 δ(ν − νL (t)) + Γ (t) . (6.363) ln 1 + M0 δ(ν − νL (t)) aν 2 ν=νL (t)

Moreover, for the photon gas (6.349) and (6.350) become lim d1 (ν, ρ) = −1 +

ρ/g→0

lim d2 (ν, ρ) = T .

ρ/g→0

2T , ν

(6.364) (6.365)


295

0.06 ρ(ν) 0.05 0.04 0.03 0.02 0.01 0

2

4

6

ν

8

10

Fig. 6.19. Stationary solution of the Bose Fokker–Planck equation (6.362). Solid line: analytical result (6.366). Diamonds: numerical results obtained by solving (6.363) using the averaging method for self-consistent Ito–Langevin equations. Parameters: T = 1.0, a = 0.1 (L = 20000, ∆t = 0.1, 2[∆x]2 = 0.1, wn via Box–Muller). A reflective boundary at νb = 0.1 was used (see also Fig. 6.17) [180]

0.14 u (ν)

0.12 0.1 0.08 0.06 0.04 0.02 0

2

4

ν

6

8

10

Fig. 6.20. Illustration of Planck’s radiation formula. Planck’s formula as obtained from (6.367) (solid line) and as obtained by solving numerically the Ito–Langevin equation (6.363) (diamonds). Parameters as in Fig. 6.19 [180]

Since the chemical potential µ of photons equals zero, the stationary solution (6.341) reads aν 2 . (6.366) ρst (ν) = exp{ν/T } − 1 The spectral energy density u(ν) of a cavity with volume V = 1 is defined by u(ν) = νρst (ν) [14, 269, 293]. Using (6.366), we obtain Planck’s radiation formula

296


u(ν) =

aν 3 . exp{ν/T } − 1

(6.367)

From (6.366) and ν ∈ Ω = [0, ∞) it follows that the total mass ∞M0 of the photon gas for a particular temperature T is given by M0 = 0 ρst (ν) dν. If we substitute this M0 -value into (6.363), we obtain a closed description of the stochastic evolution of the photon frequencies ν. In particular, ρ(ν, t) and u(ν) can be computed from ρ(ν, t) = M0 δ(ν − νL (t)) and u(ν) = M0 ν δ(ν − νL (t))st , see Figs. 6.19 and 6.20. Relativistic Fermions and Bosons In the case of quantum particles with high energies we need to account for relativistic effects. To this end, we may substitute in the quantum FokkerPlanck equation (6.346) and the quantum Langevin equations (6.354) and (6.355) the relativistic formula for the density of states of fermions and bosons given by [238, 373] g() = a( + mc2 ) ( + 2mc2 ) , (6.368) where c is the speed of light. In fact, it is clear that in the √ non-relativistic limit mc2 the density of states function reduces to g ∝ , whereas in the so-called ultrarelativistic limit mc2 quantum particles can be treated as particle waves that satisfy g ∝ 2 . For details see [184]. 6.5.7 Population Dynamics Entropy Fokker–Planck equations are in particularly tailored to describe the spread of populations. The reason for this is twofold. First, linear diffusion equations require that the diffusion velocities of individuals can become arbitrarily large [247]. For example, if we assume that v(x, t) = −c ρ−1 (x, t)∇ρ(x, t) holds (where c > 0 is a constant) and substitute this relation into (6.159), we obtain a linear diffusion equation but |v| can tend to infinity for ρ → 0. Since the dispersion velocities of humans and animals are bounded, we may assume that the relationship between v and ρ differs from v(x, t) = −c ρ−1 (x, t)∇ρ(x, t). In this case, the continuity equation yields a nonlinear evolution equation for ρ, For example, if we assume that v(x, t) = −c∇ρν with ν ≥ 1 holds, then we have v = 0 for ρ → 0 and ∇ρ → 0. As we have seen in Sect. 6.5.1, the assumption v ∝ −∇ρν leads to the porous medium equation (6.162), which in turn can be interpreted as an entropy Fokker–Planck equation. Second, solutions of the linear diffusion equation typically exhibit nonvanishing tails (see, e.g., the Gaussian solutions of Wiener processes). The population densities observed in experiments, however, resemble cut-off distributions. As shown in Sects. 6.5.2 and 6.5.3, such cut-off distributions can be


297

obtained as stationary solutions of entropy Fokker–Planck equations. Therefore, the evolution of the populations under investigation may appropriately be described by means of nonlinear Fokker–Planck equations involving general entropy and information measures. For example, Okubo et al. have suggested that the dispersal of insects can be described by means of the evolution equation ∂ ∂ ∂ ∂ (6.369) ρ(x, t)ν ρ(x, t) , ρ(x, t) = γ sgn(x)ρ(x, t) + Q ∂x ∂x ∂x ∂t for γ ≥ 0 and ν ≥ 0, where sgn(x) is the function defined by sgn(x) = 1 for x ≥ 0 and sgn(x) = −1 otherwise [455, 456]. In particular, the spatial distribution of mosquitoes within a mosquito swarm has been described by the cut-off distribution ρ(x) = a{1 − b|x|}2+ for x ∈ Ω = lR with a, b > 0 [456, Sect. 6.2.2]. This distribution corresponds to a stationary solution of (6.369) for ν = 1/2. If M0 describes the mass M0 = Ω ρ(x) dx and if we put P = ρ/M0 , then we can cast (6.369) into the entropy Fokker–Planck equation (6.170) with q = ν + 1. Note that also other ν-values for (6.369) have been considered in population dynamics [438, 635]. Furthermore, Shigesada and Teramoto [456, Sect. 5.6] and Schweitzer [515, Sect. 9.1.2] proposed nonlinear Fokker–Planck equations of the form ∂ ∂ dU0 (x) ∂2 ρ(x, t) = ρ(x, t) + 2 [α(x) + β(x)ρ(x, t)] ρ(x, t) ∂t ∂x dx ∂x

(6.370)

to describe the diffusion of populations and migration processes. For α(x) = α, β(x) = β, and P = ρ/M0 the evolution equation (6.370) corresponds to the entropy Fokker–Planck equation (6.1) involving the free energy functional F = U0 + α BS + with q = 2.

β T Sq M0

(6.371)

7 General Nonlinear Fokker–Planck Equations

This chapter is concerned with general nonlinear Fokker–Planck equations that can be cast into the form (2.4). In Sect. 7.1 we will discuss the stability of systems with one-dimensional nonlinearities. In Sect. 7.2 we will show how to treat general nonlinear Fokker–Planck equations by means of analytical tools that have been developed for free energy Fokker–Planck equations. Sects. 7.3 and 7.4 are about examples and applications. Finally, we will give some references on the topic of nonlinear Fokker–Planck equations in Sect. 7.5. Note that in this chapter we will focus on the univariate case (2.10) with coefficients that do not depend explicitly on t: ∂ ∂ ∂2 P (x, t; u) = − D1 (x, P )P + D2 (x, P )P . ∂x ∂x2 ∂t

(7.1)

7.1 Linear Stability Analysis 7.1.1 Stationary Solutions For one-dimensional nonlinearities (7.1) becomes ∂ ∂2 ∂ P (x, t; u) = − D1 (x, A)P + 2 D2 (x, A)P ∂t ∂x ∂x

(7.2)

and involves the probability current J = D1 (x, A)P −

∂ D2 (x, A)P , ∂x

(7.3)

see Sect. 2.2.4. We consider boundary conditions and coefficients D1 , D2 for which stationary distributions can be computed from J = 0 and, consequently, are given by x D1 (x , Ast ) 1 exp dx . (7.4) Pst (x) = ZD2 (x, Ast ) D2 (x , Ast ) The order parameter Ast can be determined by means of the self-consistency equation

300


Ast = R(Ast ) ,

(7.5)

where R(m) is defined by x D1 (x , m) 1 exp dx , (7.6) P (x, m) = ZD2 (x, m) D2 (x , m) x D1 (x , m)/D2 (x , m) dx dx and R(m) = with Z(m) = Ω D2−1 (x, m) exp A(x)P (x, m) dx. That is, R(m) reads explicitly x

D1 (x , m) A(x) dx dx exp D (x , m) D2 (x, m) x 2 R(m) = Ω . (7.7) 1 D1 (x , m) dx exp dx D2 (x , m) Ω D2 (x, m) 7.1.2 Stability of Stationary Solutions (Globally Nonoscillatory Instabilities) Often, the hypothesis is made that the stability of stationary distributions can be read off from the slope of R(m) at intersection points m = R(m). That is, the hypothesis is made that the implications (5.32) derived in Sect. 5.1 for several generic free energy Fokker–Planck equations also hold in the general case. In fact, one can find support for this hypothesis [186, 187]. In order to elucidate this point, we confine ourselves to studying systems with diffusion coefficients D2 (x, A) = D2 (x), for which (7.2) reads ∂2 ∂ ∂ P (x, t; u) = − D1 (x, A)P + 2 D2 (x)P . ∂t ∂x ∂x Likewise, stationary distributions are now given by x D1 (x , Ast ) 1 Pst (x) = exp dx ZD2 (x) D2 (x )

(7.8)

(7.9)

(see (7.4)) and lead to self-consistency equations Ast = R(Ast ) with x

A(x) D1 (x , m) exp dx dx D2 (x ) Ω D2 (x) x , (7.10) R(m) =

1 D1 (x , m) dx exp dx D2 (x ) Ω D2 (x) see also (7.7). From (7.10) it follows that 7 6

X D1 (x , Ast ) ∂ dR(m) = C A, dx , dm A ∂ Ast D2 (x ) st

where C describes the cross-correlation function

(7.11)

7.1 Linear Stability Analysis

C(f, g) = f gst − f st gst = (f − f st )(g − gst )st

301

(7.12)

for functions f (x) and g(x). In order to apply linear stability analysis, we consider perturbations = P −Pst with Ω (x) dx = 0 of stationary solutions Pst . Substituting P = Pst + into (7.8) and neglecting nonlinear terms with respect to , we obtain the linear evolution equation

with A =

∂ ∂ ∂2 (x, t) = − D1 (x, Ast ) + D2 (x) ∂t ∂x ∂x2 ∂D1 (x, Ast ) ∂ Pst (x) , − A

∂ Ast ∂x

A(x) (x, t) dx. Equation (7.13) can be written as ∂D1 (x, Ast ) ∂ ∂ ∂ ∂ Pst (x) D2 Pst − A

(x, t) = ∂ Ast ∂x ∂t ∂x ∂x Pst

(7.13)

Ω

(7.14)

(hint: use (7.14) as starting point and derive (7.13), see [176]). Let us apply√Shiino’s decomposition to the √ perturbation . That is, we first write (x, t) = Pst (x, t) with (x, t) = β(t) Pst φ(x) + χ⊥ (x,√ t). The function χ is assumed to be orthogonal to the first function ϕ(x) = Pst (x)φ(x): √ √ χ (x, t) P (x)φ(x) dx = 0. We also require that P χ (x, t) dx = 0 ⊥ st st ⊥ Ω Ω and Ω Pst (x)φ(x) dx = 0, which implies that Ω (x) dx = 0. We define φ(x) by

x D1 (x , Ast ) ∂ dx φ(x, Ast ) = ∂ Ast D2 (x ) C B

X D1 (x , Ast ) ∂ dx − , (7.15) ∂ Ast D2 (x ) st

which gives us (x, t) in the form of

x D1 (x , Ast ) ∂ dx (x, t) = β(t)Pst (x) ∂ Ast D2 (x ) C 7 B

X D1 (x , Ast ) ∂ + Pst (x)χ⊥ (x, t) . − dx ∂ Ast D2 (x ) st

(7.16) In what follows we assume that φ = 0 holds. From our definitions it follows that Ω AφPst dx = C and A = βC + E(χ⊥ ), where E(χ⊥ ) denotes an expression that depends on χ⊥ and C depends on the arguments as in (7.11). Consequently, substituting (7.16) into the right-hand side of (7.14), we obtain ∂D1 (x, Ast ) ∂ ∂ Pst (x) + E (χ⊥ ) , (7.17) (x, t) = β(t)(1 − C) ∂t ∂x ∂ Ast

302


where C takes the arguments as in (7.11) and E (χ⊥ ) describes terms that depend on χ⊥ and vanish for vanishingfunctions χ⊥ . Multiplying (7.17) with /Pst , and performing the integration Ω ...dx, we obtain B 2 C

2 d 1 (x, t) ∂D1 2 dx = −β (1 − C) + E (χ⊥ ) , (7.18) D2 ∂ Ast dt Ω 2Pst (x) st

where E (χ⊥ ) describes terms containing χ√ ⊥ that satisfy E (χ⊥ ) = 0 for χ⊥ = 0. Due to the orthogonalityof χ⊥ and Pst φ it follows that the equiv alence Ω 2 (x, t)/Pst (x) dx = β 2 φ2 st + Ω χ2⊥ (x) dx holds, which leads to B 2 C

2 d β 2 (t) d χ2⊥ (x, t) ∂D1 1 2 φ st dx = −β (1−C) +E (χ⊥ ) . + D2 ∂ Ast dt 2 dt Ω 2 st (7.19) 2 Note that for perturbations with χ⊥ (x, t0 ) = 0 we have d[ Ω χ⊥ (x, t) dx]/dt = 0 at t = t0 . Consequently, taking (7.11) and E (χ⊥ = 0) = 0 into account, for perturbations (x, t) that satisfy χ⊥ = 0 and β = 0 at t = t0 we obtain

2 d (x, t0 ) 1 2 d 2 φ st β (t0 ) = dx dt Ω 2Pst (x) 2 dt β=0,χ⊥ =0 B 2 C 1 ∂D1 dR 2 = −β 1 − . dm A D2 ∂ Ast st st Y

(7.20) By assumption we have φ = 0 ⇒ φ2 > 0. In addition, in what follows we will consider the case in which the expression Y does not vanish. Then, if the inequality dR(Ast )/dm > 1 (< 1) holds, the amplitude |β| of the perturbation (7.16) increases (decreases) at t = t0 . Note that on account of the relation

2 d (x, t) d dx = , (7.21) dt Ω 2Pst (x) dt

for the norm (see also Sect. 5.1.2)

f = Ω

we have d β2 |β=0,χ⊥ =0 = − dt

f2 dx Pst

(7.22)

B 2 C dR 1 ∂D1 1− . dm A D2 ∂ Ast

(7.23)

st

Consequently, for dR(Ast )/dm > 1 (< 1) the norm increases (decreases) at t = t0 for perturbations (7.16) with β = 0 and χ⊥ = 0. We consider now


303

a fundamental class of stationary distributions, namely, distributions that involve simple fixed point instabilities with respect to the norm (7.22). That is, we assume that for all possible small deviations the norm either increases or decreases. In the former case, we have an unstable fixed point distribution. In the latter case, we have an asymptotically stable fixed point distribution. Note that this requirement implies that we exclude oscillatory instabilities and saddle point instabilities from our considerations. For simple fixed point distributions the sign of 1 − dR(Ast )/dm tells us not only how a particular perturbation evolves with time but it tells us how all possible perturbations evolve. Consequently, we conclude that dR(m) < 1 ⇒ Pst asymptotically stable, dm A st dR(m) > 1 ⇒ Pst unstable. (7.24) dm A st

By similar reasoning, for stationary distributions that either describe an asymptotically stable fixed point, an unstable fixed point, or a saddle point with respect to the function space of probability densities and the norm (7.22), we conclude that dR(m) Pst asymptotically stable ⇒ 1 ⇒ Pst unstable . (7.26) dm A st

That is, for stationary distributions related to saddle point instabilities we can derived necessary (but not sufficient) conditions for asymptotically stable stationary probability densities. Comparing the result obtained so far with (5.32), we realize that by means of self-consistency equation analysis we can determine to a certain extent the stability of stationary solutions of general nonlinear Fokker-Planck equations. Globally Nonoscillatory Instabilities Let us illustrate this issue by considering a stationary distribution Pst (x) defined on Ω = lR. We assume that perturbations (x) of this distribution can be written by means of their Fourier transforms as (x, t) = Pst (x) a(k, t) exp{ikx} dk with a(−k, t) = a∗ (k, t) complex. We require that the amplitudes a(k, t) of all Fourier modes involve real Lyapunov exponents λ(k). That is, we use a(k, t) = a0 (k) exp{λ(k) t} with λ(k) real and a0 (−k) = a∗0 (k) complex. Consequently, at a bifurcation point the system exhibits a nonoscillatory behavior with respect to all Fourier modes (globally nonoscillatory instability). In this case, we find that the norm of reads

304


2 = π |a0 (k)|2 exp{2λ(k)t} dk. In addition, a stationary distribution corresponds to an asymptotically stable fixed point if λ(k) < 0 for all k, a saddle point if λ(k) > 0 for some k and λ(k) ≤ 0 for others, and an unstable fixed point2 if λ(k) > 0 for all k. Using the aforementioned relation 2 = π |a0 (k)| exp{2λ(k)t} dk, we can illustrate explicitly that the conclusions drawn in (7.24) hold if we know that we are dealing either with a stable or an unstable fixed point and that the conclusions drawn in (7.25) and (7.26) hold if the distribution Pst (x) may also correspond to a saddle point. For example, if dR(Ast )/dm > 1 holds, then from (7.23) it follows that d /dt > 0 which implies that there is at least one positive Lyapunov exponent. This, in turn, implies that Pst (x) corresponds to a saddle point or an unstable fixed point. In contrast, if Pst (x) corresponds to a stable fixed point, then we have λ(k) < 0 for all k and d /dt < 0 for all kinds of perturbations. Consequently, we have d /dt < 0 for the particular perturbation with χ⊥ = 0 and β = 0. From (7.23) it then follows that dR(Ast )/dm < 1 holds. The Role of δ 2 SB Using the relation δ 2 SB [Pst ](2 ) = − Ω 2 (x)/Pst (x) dx, which holds for the Boltzmann entropy (6.96), we can write (7.21) and (7.22) as

f2 f = dx = −δ 2 SB [Pst ](f ) (7.27) Ω Pst and

d 2 d 2 δ SB = . (7.28) dt dt From (7.20), (7.24), and (7.26) we conclude that dR(m) d δ 2 SB [Pst ]() 1 ⇒ Pst unstable. dt 2 dm A β=0,χ⊥ =0,t=t0 st (7.29) The expression dδ 2 SB [P ]/dt is known as the excess entropy production [228, 353, 449]. From (7.29) it is clear that if the excess entropy production dδ 2 SB [P ]/dt at a stationary solution Pst is negative for perturbations of the form (7.16), then the stationary distribution is an unstable one. Indeed, in nonlinear nonequilibrium thermodynamics it has been shown that for many systems dδ 2 SB /dt < 0 is a necessary condition that a stationary state becomes unstable and a nonequilibrium phase transition occurs [228, 353, 449]. For systems that can be described by means of the nonlinear Fokker–Planck equation (7.8), we can draw the conclusions that the condition dδ 2 SB /dt < 0 is a sufficient condition for instability (provided that we are dealing with a globally nonoscillatory instability). −


305

7.1.3 On an Additional Stability Coefficient∗ From (7.17) we have derived the evolution equation (7.20) that completely describes the evolution of β(t) at t = t0 in combination with the stability ˜ > 0 the amplitude |β(t)| decreases ˜ = 1 − dR(A )/dm. For λ coefficient λ st ˜ < 0 the amplitude |β(t)| increases at t = t0 . From at t = t0 , whereas for λ (7.17) we may obtain alternative stability coefficients. These coefficients will yield the same result but they may reveal some additional information about the stability problem. Multiplying (7.17) with A(x), integrating with respect to x and using partial integration (under the assumption that the surface term vanishes that occurs due to partial integration), we obtain

d ∂χ⊥ (x, t0 ) C β(t0 ) + Pst (x)A(x) dx dt ∂t Ω Y J I dA ∂D1 (X, Ast ) = (C − 1)β(t0 ) , (7.30) dX ∂ Ast st for perturbations with χ⊥ (x, t) = 0 and β = 0 at t = t0 . If there are perturbations (7.16) for which the contribution χ⊥ (x,√t) evolves in a subspace of the √ function space, which is orthogonal to A(x) P st (and orthogonal to φ(x) P st ; see the preceding), then we have

χ⊥ (x, t)A(x) Pst (x) dx = 0 , (7.31) Ω

for t ≥ t0 and, consequently, the term Y in (7.30) vanishes. Considering C = dR(Ast )/dm = 0 and using (7.11), we obtain ⎛ 6 7−1 ⎞ J I dR(m) d dA ∂D1 (X, Ast ) ⎝1 − ⎠ β(t0 ) , (7.32) β(t0 ) = dt dX ∂ Ast dm A st st

which can be written as dR(m) δ d 1− β(t) = − β(t) dR(Ast )/dm dm A dt st ⎛ 6 7−1 ⎞ dR(m) ⎠ β(t) , = δ ⎝1 − dm A

(7.33)

st

by introducing the stability coefficient δ defined by [187] I J dA ∂D1 (X, Ast ) δ= . dX ∂ Ast st

(7.34)

306


Multiplying (7.33) with β(t) and comparing the result with (7.20), we find B 2 C 1 1 ∂D1 dR(m) δ= 2 , (7.35) φ st D2 ∂ Ast dm A st st >0

which implies that δ and dR(Ast )/dm may differ in magnitude but they have the same sign. We may evaluate δ in order to determine the stability of stationary solutions. However, as argued earlier, in doing so, we cannot gain information about the stability problem at hand that goes beyond the information contained in (7.25) and (7.26). That is, we still cannot say more than that the implications (7.25) and (7.26) hold. An issue that seems to be of interest with regard to the coefficient δ is the conditions under which δ becomes relevant at all. For example, let us assume that there is a function f (z) such that

x D1 (x , Ast ) ∂ dx A(x)f (Ast ) = (7.36) ∂ Ast D2 (x ) holds. Then, √ (7.31) is satisfied because χ⊥ satisfies by definition the relation χ (x, t) Pst (x)φ(x) dx = 0 and we have φ(x) ∝ A(x). As we will see in Ω ⊥ Sect. 7.2.3, the relation (7.36) describes a matching condition for which local Lyapunov functionals can be derived.

7.2 Free Energy and Lyapunov Functional Analysis In some cases, nonlinear Fokker–Planck equations of the form (7.1) can be studied by means of methods that have been developed for free energy Fokker–Planck equations. The idea is to transform a given nonlinear Fokker– Planck equation into a nonlinear Fokker–Planck equation that can be studied by means of free energy measures and Lyapunov functionals. Table 7.1 summarizes the problems and remedies that we will discuss in what follows. Note that there is no guarantee that these transformations lead to success. That is, we present here a toolbox containing techniques that lead in some cases to the desired result but may fail in other cases. In addition, we would like to point out that nonlinear Fokker–Planck equations with multiplicative noise terms may be regarded as free energy Fokker–Planck equations with state-dependent mobility coefficients as demonstrated in Sect. 5.1.7. 7.2.1 Moving Frame Transformations We consider here (2.10) for D1 (x, t, P ) = −γx + F (t) − d[ Ω UMF (x − ˆ s (P ), S = s(P ) dx, γ ≥ 0, and x )P (x ) dx ]/dx and D2 (x, t, P )P = QL Ω UMF (z) = UMF (−z), which reads

7.2 Free Energy and Lyapunov Functional Analysis

307

Table 7.1. Treatment of nonlinear Fokker–Planck equations (NLFPEs) using free energy measures and Lyapunov functionals Problem Free energy FPE NLFPE with with F not bounded D2 (P )

NLFPE with D1 (x, A)

NLFPE with D1 (x, P ), D2 (P )

Remedy

moving frame transformation

derivation of entropy/ information measures

derivation of local Lyapunov functional

derivation of Lyapunov functional

Result

free energy FPE with F bounded

free energy FPE stability analysis by means of Lyapunov’s direct method

NLFPE involving a Lyapunov functional

∂ ∂ ∂ γx − F (t) + UMF (x − x )P (x , t; u) dx P P (x, t; u) = ∂x ∂x Ω ∂t ∂2 ˆ +Q 2 L (7.37) s (P ) , ∂x ˆ s is defined by (4.6) and acts on the entropy kernel s(z). Equation where L (7.37) can be regarded as a special case of the nonlinear Fokker–Planck equation (4.7) supplemented with an explicitly time-dependent drift force F (t). Using (4.55), the nonlinear Fokker–Planck equation (7.37) can be written as

∂ ∂ ∂ γx − F (t) + UMF (x − x )P (x , t; u) dx P P (x, t; u) = ∂t ∂x ∂x Ω ∂ δS ∂ . (7.38) −Q P ∂x ∂x δP We consider probability densities P (x, t; u) subjected to periodic boundary conditions (with γ = 0, x ∈ Ω = [a, b] and UMF (z) = UMF (z + T ) with b − a = T > 0) and natural boundary conditions (with x ∈ Ω = lR). Solutions P (x, t; u) of (7.38) can be studied in a moving frame described by the coordinate y satisfying y = x − g(t) . (7.39) The probability density P in the moving frame (or moving coordinate system) is given by P (y, t)dy = P (x, t; u)dx and P (y, t) = P (y + g(t), t; u) ,

(7.40)

308


because we have dx = dy [498]. Let us choose g(t0 ) = 0 such that P (x, t0 ) = P (x, t0 ; u) = u(x) .

(7.41)

Then, we have

d ∂ ∂ ∂ , (7.42) P (y, t) = P (x, t; u) g(t) + P (x, t; u) ∂t ∂x ∂t y+g(t) dt y+g(t) ∂ ∂ P (y, t) = P (x, t; u) , (7.43) ∂y ∂x y+g(t) ∂2 ∂2 P (y, t) = P (x, t; u) . (7.44) 2 2 ∂y ∂x y+g(t)

From (4.55) the relation

ˆ s ∂ 2 P ˆ s ∂P 2 ∂ ∂ δS ∂2 ˆ dL d2 L P = + Ls (P ) = dz 2 ∂x dz ∂x2 ∂x ∂x δP ∂x2

(7.45)

P

P

can be derived which, in turn, can be evaluated at x = y + g(t): ˆ s ∂ 2 P ˆ s ∂P 2 ∂ dL ∂ δS d2 L P + = dz ∂x2 dz 2 ∂x ∂x ∂x δP y+g(t) P

∂ ∂ δS = . P ∂y ∂y δP

P

y+g(t)

(7.46)

Let us write (7.38) as ∂ ∂ P (x, t; u) = γP + [γx − F (t)] P ∂t ∂x

∂ ∂ δS ∂ ∂ . (7.47) P UMF (x − x )P (x , t; u) dx − Q P + ∂x ∂x Ω ∂x ∂x δP If we substitute (7.47) into the right-hand side of (7.42), we obtain ∂ dg(t) ∂ P (y, t) = γP + γx − F (t) + P ∂t dt ∂x

∂ ∂ ∂ ∂ δS + P UMF (x − x )P (x , t; u) dx − Q P . ∂x ∂x Ω ∂x ∂x δP y+g(t) (7.48) Replacing x by y + g(t) and x by y + g(t) and using (7.43) and (7.44), we find ∂ ∂ dg(t) ∂ P (y, t) = − F (t) + γg(t) P (y, t) + γyP (y, t) ∂t dt ∂y ∂y

∂ ∂ ∂ δS d + P UMF (y − y )P (y, t) dy − Q P . (7.49) ∂y dy Ω ∂y ∂y δP


309

Finally, let us put

t

g(t) =

exp{−γ(t−z)}F (z) dz ,

(7.50)

t0

which implies that the probability densities P and P satisfy the relation

t P (y, t) = P y + e−γ(t−z) F (z) dz, t; u (7.51) t0

and that dg/dt = −γg + F (t) holds. Then, (7.49) reduces to

∂ d ∂ γy + UMF (y − y )P (y, t) dy P P (y, t) = ∂t ∂y dy Ω ∂ ∂ δS . −Q P ∂y ∂y δP

(7.52)

Note that for natural boundary conditions the phase space Ω in the moving frame description is the same as in the original problem described by (7.38). The reason for this is that for natural boundary conditions the transformation x → y = x − g(t) for finite g(t) does not affect Ω = lR. For periodic boundary conditions we require that γ = 0 holds and that UMF (z) be a periodic function. Due to the moving frame transformation the phase space Ω = [a, b] is shifted to Ω (t) = [a − g(t), b − g(t)]. However, on account of our requirement all quantities involved in (7.52) are periodic functions, which implies that at every time point t we can shift Ω by an arbitrary constant without changing the behavior of the solution. Therefore, we may shift Ω (t) back to Ω. In fact the transformation Ω (t) → Ω has tacitly been carried out to obtain (7.49-7.52). Using the free energy functional

1 γ 2 y P (y) dy + UMF (y − y ) dy dy − QS[P ] , (7.53) F [P ] = 2 Ω 2 Ω Ω the evolution equation (7.52) can be cast into the free energy Fokker–Planck equation ∂ ∂ ∂ δF P (y, t) = P (y, t) . (7.54) ∂t ∂y ∂y δP In sum, by means of the moving frame transformation (7.51), the nonlinear Fokker–Planck equation (7.38) becomes a free energy Fokker–Planck equation defined by (7.53) and (7.54). Example Let us illustrate the moving frame transformation for the special case F (t) = ω = constant that is frequently discussed in the literature. For example, for

310


a periodic random variable X ∈ Ω ∈ [0, 2π] and t ≥ 0 we may consider the nonlinear Fokker–Planck equation

d ∂ ∂ ∂ P (x, t; u) = − ω− UMF (x − x )P (x , t; u) dx P + Q 2 P . ∂t ∂x dx Ω ∂x (7.55) From (7.51), γ = 0, and F (t) = ω it follows that P (y, t) = P (y + ω(t − t0 ), t; u) .

(7.56)

Using (7.56), the evolution equation (7.55) can be written as [365]

∂ ∂2 ∂ d P (y, t) = P UMF (y − y )P (y, t) dy + Q 2 P . (7.57) dy Ω ∂y ∂t ∂y 7.2.2 Derivation of Entropy and Information Measures In Sect. 4.5.2 we have shown that by means of the transformation (4.58), we can write the free energy Fokker–Planck equation (4.49), ∂ δF P (x, t; u) = −∇ · [I(x, t, P ) P ] + ∇ · M(x, t, P )P · ∇ , (7.58) ∂t δP in terms of the nonlinear Fokker–Planck equation (2.4), ∂ ∂ P (x, t; u) = − Di (x, t, P )P (x, t; u) ∂xi ∂t i=1 M

+

M i,k=1

∂2 Dik (x, t, P )P (x, t; u) . ∂xi ∂xk

(7.59)

The question now arises: to what extent is this transformation invertible? In other words, at issue is to find a mapping that transforms the nonlinear Fokker–Planck equation (7.59) into the free energy Fokker–Planck equation (7.58). In general, such a mapping will not exist. However, in some cases, we can indeed associate entropy and energy functionals to nonlinear Fokker– Planck equations and, in doing so, cast them into the form of free energy Fokker–Planck equations [190]. In what follows, we confine ourselves to discussing the univariate nonlinear Fokker–Planck equation (2.10) for the special case ∂ ∂ ∂2 P (x, t; u) = − D1 (x, P )P (x, t; u) + D2 (P )P (x, t; u) , ∂t ∂x ∂x2

(7.60)

where D1 can be derived from an internal energy functional D1 (x, P ) = −

d δU dx δP

(7.61)


311

and D2 (z) is a function of z. That is, D2 (P ) does not denote a functional of P . We assume that D2 (P ) involves a proportional constant Q > 0 that can be regarded as an overall noise amplitude and decompose D2 (P ) as follows D2 (P ) = QD2 (P ) .

(7.62)

Our objective is to transform (7.60) into (4.7) for an entropy and information measure given by S[P ] = Ω s(P ) dx. Requiring the equivalence between (7.60) and the free energy Fokker–Planck equation (4.7) for a univariate random variable, we need to determine s such that ˆ s (P ) D2 (P )P = L

(7.63)

ˆ s defined by (4.6) satisfies holds. Since L ˆ s (z) = s − z ds = −z 2 d s(z) , L dz dz z

(7.64)

the relation (7.63) becomes d s(P ) D2 (P ) =− , P dP P

(7.65)

which gives us our final result

P

s(P ) = −P P0

D2 (z) P dz + s0 . z P0

(7.66)

ˆ f (z) vanishes for linear functions (i.e., we have f (z) = az ⇒ L ˆ f (z) = Since L ˆ 0), the lower boundary P0 is irrelevant for the expression Ls (P ). Therefore, we write (7.60) as ∂ ∂ ∂2 ˆ P (x, t; u) = − D1 (x, P )P + Q 2 L s (P ) , ∂x ∂x ∂t

P D2 (z) s(P ) = −P dz . z

(7.67)

Alternatively, we may write (7.67) as ∂ ∂ ∂ ∂ δS P (x, t; u) = − D1 (x, P )P + Q P , ∂t ∂x ∂x ∂x δP

P (x) D2 (z) P (x) dz dx . S[P ] = S0 − z Ω

(7.68)

In deriving this result we have made use of (4.55) and have exploited s0 and P0 to add an offset S0 to the entropy S[P ] = Ω s(P ) dx. Taking the drift term (7.61) into account, we realize that (7.68) can be written as

312


∂ ∂ δF ∂ P (x, t; u) = P ∂t ∂x ∂x δP

(7.69)

with the free energy functional F = U [P ]−QS[P ]. We will return to the relationship between the evolution equations (7.60), (7.68), (7.69) in Sect. 7.2.4. Let us conclude this section with an example. Let us consider the nonlinear Fokker–Planck equation ∂2 ∂ P (x, t; u) ∂ , P (x, t; u) = − h(x)P (x, t; u) + Q 2 ∂x ∂x 1 + αP (x, t; u) ∂t for α ≥ 0. From D2 (P ) = 1/(1 + αP ) and (7.66) we obtain

P P 1 s(P ) = −P dz = −P ln z(1 + αz) 1 + αP

(7.70)

(7.71)

and the entropy

Sα [P ] = −

NSF

P (x) ln Ω

P (x) dx + S0 1 + αP (x)

(7.72)

addressed in Sect. 6.4.2. The relevance of this entropy and information measure will be discussed in Sect. 7.4.4. 7.2.3 Derivation of Local Lyapunov Functionals Ito Case We study next (7.8) for drift terms that are linear with respect to the order parameter A such that we have D1 (x, A) = h(x) − κ (A(x) − A(X))

(7.73)

and ∂ ∂ ∂2 P (x, t; u) = − [h(x) − κ (A(x) − A(X))] P + D2 (x)P ∂t ∂x ∂x2

(7.74)

with κ > 0. We refer to (7.74) as the Ito case of a nonlinear Fokker–Planck equation. The Stratonovich case will be defined below, see also Sect. 2.2.2. We will analyze the stability of stationary solutions. To this end, we will proceed as in Sect. 7.1.2. While in Sect. 7.1.2, we have excluded oscillatory instabilities from our considerations, we will derive here some more rigorous results. By means of (7.4), stationary solutions of (7.74) can be written as x

x h(x ) − κA(x ) 1 1 , Pst (x) = + κ A exp dx dx st ZD2 (x) D2 (x ) D2 (x ) (7.75)


313

where Z denotes a normalization constant. In line with our remark in Sect. 7.1.1 note that this result holds, for example, for natural and periodic boundary conditions. In the latter case, however, we need to require that h, A, D be defined in such as way that P (x + T ) = P (x) holds, where T is the period of the process under consideration. By virtue of x 1 h(x ) − κ[A(x ) − m] P (x, m) = , exp dx Z(m)D2 (x) D2 (x )

R(m) = A(x)P (x, m) dx , (7.76) Ω

we define the self-consistency equation m = R(m), whose solutions determine the stationary order parameter values Ast occurring in (7.75). Differentiation of R(m) with respect to m gives us

x 1 dR(m) dx , (7.77) = κC A(x), D2 (x ) dm A st

where C(f, g) is defined by (7.12). Substituting P = Pst + into (7.74), the evolution equation for the perturbation is found as ∂ ∂ ∂2 (x, t) = − [h(x) − κ (A(x) − Ast )] + 2 D2 (x) ∂t ∂x ∂x

dP st . −κ A(x )(x ) dx dx Ω Using (7.75), we can transform (7.78) into

∂ ∂ ∂ dPst , (x, t) = D2 (x)Pst −κ A(x )(x , t) dx ∂x Pst dx ∂t ∂x Ω

(7.78)

(7.79)

which corresponds to (7.14) for systems with drift coefficients (7.73). Let us write (7.79) as

x

∂ ∂ 1 ∂ (x, t) = dx D2 (x)Pst . − κ A(x ) (x , t) dx ∂t ∂x ∂x Pst D2 (x ) Ω (7.80) If we consider now functions A(x) and diffusion coefficients D2 (x) that satisfy

x 1 (7.81) A(x) = c dx D2 (x ) (where c is a constant) and introduce the functional Ψ [P ] = or, alternatively, the functional

κ KA (X) − BS[P ] , 2c

(7.82)

314


Ψ [P ] = −

κ 2 A − BS[P ] , 2c

then (7.80) can equivalently be expressed as

∂ ∂ δ 2 Ψ [Pst ] ∂ (x, t) = D2 (x)Pst (y, t) dy . ∂t ∂x ∂x Ω δP (x)δP (y)

(7.83)

(7.84)

Having obtained (7.84), we can proceed as in Sect. 5.1.2. Analogously to the derivation of (5.23) and (5.25), we can show that for L = δ 2 Ψ [Pst ]()/2 the relations d 2 d 2 (7.85) δ Ψ ≤0, δ Ψ = 0 ⇔ δ 2 Ψ [Pst ]() = 0 dt dt hold. The second variation δ 2 Ψ can be evaluated as demonstrated in Sect. 5.1.5 for the KA -model. Thus, we obtain a stability condition similar to the one listed in the second column of Table 5.1. If ˜ = 1 − κ KA,st (X) (7.86) λ c is positive, then we have δ 2 Ψ > 0 for = 0 and δ 2 Ψ corresponds to a Lyapunov functional that decreases with time and converges to zero in the long time limit. Consequently, perturbations vanish in the long time limit and Pst ˜ < 0, corresponds to an asymptotically stable distribution. Conversely, if λ 2 then there exists a perturbation (x) such that δ Ψ [Pst ]() < 0 and, consequently, Pst is unstable. Note that Ψ does not determine the global behavior of (7.74), that is, the solutions P (x, t; u). Rather δ 2 Ψ determines the local behavior of (7.74). That is, it determines the evolution of perturbations of stationary distributions Pst . Therefore, we may say that δ 2 Ψ describes a local Lyapunov functional. Note also that δ 2 Ψ can be regarded as a modification of the excess entropy term δ 2 SB discussed in Sect. 7.1.2. Using the matching condition (7.81), the stationary distribution (7.75) and the self-consistency equation (7.76) read x 22 1 dA dA κ1 1 A(x) − Ast (7.87) Pst (x) = h(x ) dx − exp cZ dx c dx 2c and

x 1 dA κ 2 dA P (x, m) = exp [A(x) − m] , h(x ) dx − cZ(m) dx dx 2c

R(m) = A(x)P (x, m) dx , (7.88) Ω

which eventually leads to dR/dm = κKA,st (X)/c at m = Ast . As a result, we conclude that for dR(Ast )/dm < 1 stationary distributions are asymptotically stable and for dR(Ast )/dm > 1 stationary distributions are unstable. Note that this is in line with the stability analysis by means of self-consistency equations, see Sect. 5.1.3.


315

Stratonovich Case In order to study noise induced phenomena, it is often more appropriate to consider Fokker–Planck equations such as ∂ ∂ ∂ ∂ P (x, t; u) = − [h(x) − κ (A(x) − A(X)P )] P + g(x) g(x)P , ∂t ∂x ∂x ∂x (7.89) with g(x) > 0. For κ = 0 the nonlinear Fokker–Planck equation (7.89) describes a stochastic process defined by the Stratonovich–Langevin equation [498] d (7.90) X(t) = h(X) + g(X)Γ (t) . dt Stratonovich Using D2 (x) = g 2 (x), we can cast (7.89) into the form of (7.74): 1 dD2 (x) ∂ ∂ ∂2 − κ (A(x)−AP ) P + P (x, t; u) = − h(x) + D2 (x)P . ∂t ∂x 2 dx ∂x2 (7.91) If (7.91) is a strongly nonlinear Fokker–Planck equation, then the Ito– Langevin equation corresponding to (7.91) reads d 1 dD2 (X) X(t) = h(X) + − κ [A(X) − A] + D2 (X)Γ (t) dt 2 dx Ito

(7.92)

and transition probability densities are defined by (see Chap. 3): ∂ P (x, t|x , t ; u) = ∂t : 9 1 dD2 (x) ∂ h(x) + − − κ A(x)−AP (x,t;u) P (x, t|x , t ; u) ∂x 2 dx ∂2 + 2 D2 (x)P (x, t|x , t ; u) . (7.93) ∂x Consequently, (7.92) is the Ito–Langevin equation of the Stratonovich Fokker– Planck equation (7.89). Comparing (7.91) with (7.74), we find that we need to replace h by h + 0.5dD2 (x)/dx, that is, we need to add the so-called spurious drift term 0.5dD2 (x)/dx. Using h → h + 0.5dD2 (x)/dx and the matching condition (7.81), the stationary distribution (7.75) and the self-consistency equation (7.76) become 0 x 22 1 1 dA dA κ1 A(x) − Ast Pst (x) = (7.94) h(x ) dx − exp Z c dx dx 2c

316


and 0

1 dA 1 P (x, m) = exp Z(m) c dx

R(m) = A(x)P (x, m) dx .

x

h(x )

dA κ 2 [A(x) − m] dx − dx 2c

, (7.95)

Ω −1 Comparing (7.87) and (7.94), we realize that the factor √ 1/D2 = c dA/dx in front of the exponential function is replaced by 1/ D2 . An example of a Stratonovich nonlinear Fokker–Planck equation involving a local Lyapunov functional will be given in Sect. 7.3.2.

Generalization The results obtained so far can be generalized to the nonlinear Fokker–Planck equation (7.8). As shown in Sect. 7.1.2 perturbations of stationary states satisfy (7.14). Equation (7.14), in turn, can be written as

x ∂ ∂ D1 (x , Ast ) ∂ ∂ , (7.96) − A

dx (x, t) = D2 Pst ∂t ∂x ∂x Pst ∂ Ast D2 (x ) which generalizes (7.80). Assuming that there is a function f (z) such that the matching condition (7.36) holds, we write (7.96) as ∂ ∂ ∂ (x, t) = D2 Pst (7.97) − A(x)f (Ast ) A . ∂t ∂x ∂x Pst Using B(z) with f (z) = −

d2 B dz 2

(7.98)

and Ψ [P ] = B(A) − BS[P ] ,

(7.99)

we can transform (7.97) into (7.84). Consequently, (7.85) holds and the stability coefficient can be obtained in analogy to the B(A)-model discussed in Sect. 5.1.5. We have d2 B ˜ λ = 1 + KA,st (X) . (7.100) dm2 A st

˜ > 0 we find that δ 2 Ψ [Pst ]() is a local LyaFor stationary solutions with λ punov functional and that the distributions correspond to asymptotically ˜ < 0, we have stable ones. In contrast, for a stationary solution Pst with λ 2 2 δ Ψ < 0 for = 0. Since we have dδ Ψ/dt ≤ 0 the function |δ 2 Ψ | increases as long as is small, which indicates that Pst describes an unstable stationary solution.


317

Note that in the case (7.73), the matching condition (7.36) reads x special D2−1 (x ) dx , which implies that f is independent of A A(x)f (Ast ) = κ and corresponds to a constant. If we put f = κ/c, we reobtain (7.81). From f = κ/c it follows that B(z) = −κz 2 /(2c) and the Lyapunov functional (7.99) reduces to the special case (7.83). Likewise, the stability coefficient (7.100) recovers the special case given by (7.86). 7.2.4 Derivation of Lyapunov Functionals We discuss now how to derive Lyapunov functionals for nonlinear Fokker– Planck equations [166]. Such Lyapunov functionals are monotonically decreasing functions for the solutions of nonlinear Fokker–Planck equations. They are bounded from below and become stationary if and only if we are dealing with stationary solutions of the nonlinear Fokker–Planck equations, see (4.3). They can be used to show that an H-theorem holds and that transient solutions converge to stationary ones, see Sect. 4.3. In addition, they may be used to determine the stability of stationary distributions, see Sect. 5.1. We consider a nonlinear Fokker–Planck equation of the form ∂ ∂ ∂ P (x, t; u) = − M (x, P ) (h(x) + k[x, P ]) P − L(P ) . (7.101) ∂t ∂x ∂x j Equation (7.101) involves a probability-dependent diffusion coefficient L(P ), a probability-independent drift force h(x), and a probability-dependent drift coefficient k[x, P ]. Here, L(z) is a function of z, whereas k[x, P ] is a functional of P and may also depend explicitly on the state variable x. Here, M denotes a probability-dependent mobility and we require M > 0. Note also that we have introduced above a mobility-independent probability current j. Equation (7.101) can be cast into the form (2.10) using D1 (x, P )P = M (x, P )(h(x) + k[x, P ])P − L(P )

∂ M (x, P ) , ∂x

D2 (x, P )P = M (x, P )L(P ) .

(7.102)

In general, Fokker–Planck equations such as given by (7.101) have multiple stationary solutions, see Chap. 2.4. Here, we require the existence of at least one stationary solution Pst and that in the stationary case the mobilityindependent probability current j vanishes. That is, Pst satisfies (h(x) + k[x, Pst ]) Pst (x) =

∂ L(Pst ) . ∂x

(7.103)

x h(x ) + Note that from (7.103) it follows that the integral relation P k[x .Pst ] dx = [z −1 dL/dz] dz holds, which implies that for periodic

318


x boundary conditions we need to require that the integral h(x )+k[x .Pst ] dx ˜ be a periodic function with respect to x. For M (z) = 1, k[x, P ] = k(x), and L(P ) = Q P with Q > 0, the nonlinear Fokker–Planck equation (7.101) recovers the linear Fokker–Planck equation : ∂ ∂2 ∂ 9 ˜ h(x) + k(x) P + Q 2P . P (x, t; u) = − ∂t ∂x ∂x

(7.104)

In what follows, we assume that there exists a limiting case in which (7.101) reduces to a linear evolution equation of the form (7.104). We denote this limiting case as “lin-lim”. For example, the Plastino–Plastino Fokker–Planck equation related to the entropy TSq becomes linear for q → 1, see Sect. 6.5.2. We can then define k˜ and the fluctuation strength Q in (7.103) by 1 ˜ lin-lim L(P ) . k(x) = lin-lim k[x, P ] , Q = P

(7.105)

By means of the functional

x N [x, P ] = −

k[x , P ]P (x , t; u) dx + L(P ) ,

(7.106)

the nonlinear Fokker–Planck equation (7.101) can be expressed as ∂ ∂ ∂ P (x, t; u) = − M (x, P ) h(x)P − N [P ] . ∂t ∂x ∂x

(7.107)

Introducing the functional

1 f [w] = exp Q

x

d N [x , w] 1 dx w(x ) dx

(7.108)

that acts on a probability density w(x), we obtain ∂ ln f [P ] 1 ∂N[x, P ] = , ∂x QP ∂x d ln f [Pst ] 1 dN[x, Pst ] h(x) = = , dx QPst dx Q

(7.109) (7.110)

and ∂ ∂ ∂ f [P ] P (x, t; u)M (x, P ) . P (x, t; u) = ln ∂t ∂x ∂x f [Pst ]

(7.111)

Let us dwell on the functional f for a moment. From (7.110) it follows that f [Pst ] =

1 W (x) Z

(7.112)


319

holds, where Z > 0 is an constant and W describes the Boltzmann xintegration distribution of V = − h(x ) dx defined by W (x) =

exp{− V (x)/ Q} . exp{− V (x )/ Q} dx Ω

(7.113)

For the univariate case of the free energy Fokker–Planck equation (4.7), we have k[x, P ] = −dδUNL [P ]/δP dx and ∂L(P )/∂x = P −1 ∂δS[P ]/δP ∂x and have 1 G[w] = f [w] , (7.114) e where G is defined by (4.112). That is, f [w] is a generalization of the distortion functional G[w] discussed in Sect. 4.7.1. The form of (7.111) suggests that the functional

f [P ] ∂P ln DI[P, Pst ] = dx (7.115) f [Pst ] ∂t Ω is smaller than or equal to zero for solutions of (7.111). In fact, substituting (7.111) into (7.115), integrating by parts, and assuming that the surface term thus obtained vanishes, we obtain 2

f [P ] ∂ ln DI[P, Pst ] = − P (x, t; u)M (x, P ) dx ≤ 0 . (7.116) ∂x f [Pst ] Ω Note that for periodic boundary conditions the aforementioned surface term vanishes provided that k[x, P ] is defined such that f is a periodic function with respect to x. On the basis of (7.115), we can make an attempt to cont struct a monotonically decreasing functional given by I = DI(t ) dt :

t I[P, Pst ] = ⇒

dt

f [P ] ∂P dx ln f [Pst ] ∂t Ω

d I[P, Pst ] = DI[P, Pst ] ≤ 0 . dt

(7.117) (7.118)

In the limiting case in which the nonlinear Fokker–Planck equation (7.101) ˜ becomes linear (i.e., if the limits M (z) → 1, k[x, P ] → k(x), and L(z) → Qz hold) the functional (7.108) reduces to

1 x˜ (7.119) lin-limf [w(x)] = w(x) exp − k(x ) dx Q and (7.118) yields

d ∂P P P dx = dx ln P ln Pst ∂t dt Ω Pst Ω

P ⇒ lin-lim I[P, Pst ] = I0 + dx , (7.120) P ln P st Ω d lin-lim I[P, Pst ] = dt

320


where I0 denotes an arbitrary integration constant F and the normalization condition was taken into account (i.e., d Ω P dx dt = 0). We realize that the functional I recovers in the linear limit the Boltzmann–Kullback measure Moreover, from (7.113) and (7.119) we obtain Pst (x) = exp{[−V (x)+ (4.123). x˜ k(x ) dx ]/Q}/Z , where Z is a normalization constant. The question now arises whether or not the functional (7.117) satisfies the conditions listed in (4.29) and can be used to show that transient solutions P (x, t; u) become stationary in the long time limit. In any case, I is constant in the stationary case, that is, ∂P / ∂t = 0 ⇒ dI/ dt = 0. In order to verify the boundedness of I and the implication dI/ dt = 0 ⇒ ∂P / ∂t = 0, we need to eliminate the expression ∂P / ∂t in (7.117). To this end, we write (7.118) as

d ∂P ∂P I[P, Pst ] = dx − lnf [P ] lnf [Pst ] dx . (7.121) dt ∂t ∂t Ω Ω Next, we integrate (7.109) and (7.110) with respect to x and substitute the results into (7.121). Thus, we obtain I[P, Pst ] = I[P ] with 1 (7.122) V (X) + INL [P ] , Q x

∂ d 1 1 ∂P dx dx N [x , P ] . INL [P ] = dt Q Ω ∂t P (x , t; u) ∂x (7.123) I[P ] =

In the following, we will illustrate how to derive explicit expressions for the nonlinear part INL . To this end, we will consider free energy and entropy Fokker–Planck equations for which we know that Lyapunov functionals in terms of free energy measures exist. Free Energy Fokker–Planck Equations with Boltzmann Statistics In order to study systems with linear diffusion we set M (x, P ) = 1 and x terms, k[x , P ]P (x ) dx + Q P . Then, L(P ) = Q P , which implies N [x, P ] = − (7.122) and (7.123) read 1 V (X) − BS[P ] + I1 [P ] , Q x

d 1 ∂P I1 [P ] = − dx dx k[x , P ] , dt Q Ω ∂t

I[P ] =

(7.124) (7.125)

where BS denotes the Boltzmann entropy (6.96) in the univariate case: S[P ] = − Ω P ln P dx.

B

Bounded Potential Model In the case of the bounded potential model (5.83), we have


k = kMF [x, P ] =

dB(A) dA(x) . d A dx

Consequently, the right hand side of (7.125) reads

1 dB(z) 1 d ∂P RHS = − dx = B(A) . A(x) ∂t Q dt Q dz z=A Ω

321

(7.126)

(7.127)

Then, the functional I reads I[P ] =

V (X) + B(X) − BS[P ] . Q

(7.128)

The expression V (x) + B(X) may be interpreted as the internal energy U of the system under consideration. Then, F = QI = U − Q BS can be regarded as a free energy measure, which is indeed the Lyapunov functional of the bounded potential model (5.83), see Sect. 5.1.5. Kuramoto–Shinomoto–Sakaguchi Model For the KSS model (5.210), we have Ω = [0, 2π], V = 0, k[x, P ] = −d[ Ω UMF (x − x )P (x ) dx ]/dx and UMF (z) = UMF (−z). Therefore, we can cast (7.125) into the form

d 1 ∂P (x, t; u) UMF (x−x ) dx dy . P (y, t) (7.129) I1 [P ] = dt Q Ω Ω ∂t Due to the symmetry of UMF , we obtain

1 1 P (x)P (x )UMF (x−x ) dx dx − BS[P ] . I[P ] = Q 2 Ω Ω (7.130) That is, we reobtain the result derived in Sect. 5.3.2, namely, that the KSS model F = QI = U − Q BS with U = involves the Lyapunov functional 0.5 Ω Ω P (x)P (x )UMF (x−x ) dx dx . General Case For k[x, P ] = −∂δUNL [P ]/δP ∂x the integral relation (7.125) reads

d ∂P δUNL [P ] 1 dx , I1 [P ] = dt Q Ω ∂t δP

(7.131)

which implies that I1 = UNL /Q and I[P ] =

V (X) + UNL − BS[P ] . Q

(7.132)

322


Consequently, the functional (7.131) is a possible candidate for a Lyapunov functional of the nonlinear Fokker–Planck equation ∂ ∂ ∂ δUNL [P ] ∂ P (x, t; u) = − M (x, P ) h(x) − P −Q P . ∂t ∂x ∂x δP ∂x (7.133) In fact, (7.133) is a free energy Fokker–Planck equation with F = QI, which implies that I and F correspond to Lyapunov functionals provided that they are bounded from below. Entropy Fokker–Planck Equations We address here two closely intertwined approaches to entropy Fokker–Planck equations. Entropy Fokker–Planck Equations Derived from Linear Nonequilibrium Thermodynamics Let us consider the univariate entropy Fokker–Planck equation (6.4) for mea sures S = Ω s(P ) dx, which reads ∂ ∂ ∂ ˆ (7.134) P (x, t; u) = − M (x, P ) h(x)P − Q Ls (P ) . ∂t ∂x ∂x ˆ s [P ], By comparison with (7.101), we obtain k[x, P ] = 0 and L(P ) = QL ˆ which implies N [P ] = QLs [P ], see (7.106). In this case, on account of the relation

x ∂ ˆ 1 ds(z) Q , (7.135) Ls [P (x , t)] dx = −Q P (x , t) ∂x dz P (x,t;u) we find that (7.123) reads d INL [P ](t) = dt

Ω

∂P ds(z) dx , ∂t dz P (x,t;u)

(7.136)

which implies INL [P ] = S[P ] + S0 ,

(7.137)

where S0 is an arbitrary integration constant. From (7.122) it then follows that 1 (7.138) I[P ] = V (X) − S[P ] − S0 . Q That is, I[P ] is a promising candidate for a Lyapunov functional of (7.134). In fact, in Sect. 4.5.7, we have shown that for S0 = 0 the expression F = QI = V (X)−QS[P ] corresponds to a Lyapunov functional of the nonlinear Fokker–Planck equation (7.134).


323

Entropy Fokker–Planck Equations Derived from the Kinetical Interaction Principle Let us consider stochastic processes described by the generalized Fokker– Planck equation ∂ ∂ ∂ P (x, t; u) = − P M (x, P ) h(x) − Q ln κ(P ) , (7.139) ∂t ∂x ∂x where κ(z) is a monotonically increasing function. Equation (7.139) may be regarded as the Smoluchowski limit [498] of the generalized Fokker–Planck equation derived by Kaniadakis [323] by means of the kinetical interaction principle. According to the kinetical interaction principle, the function κ describes how transition probability densities depend on process probability densities P . In the absence of such a dependency we obtain κ(z) = z. Then, for M = 1 the entropy Fokker–Planck equation (7.139) becomes linear with respect to P . Comparing (7.139) with the Fokker–Planck equation (7.101), identifications: k[x, P ] = 0 and x we can make the following dx P (x , t) ∂ ln κ(P (x , t))/ ∂x . From (7.106) and (7.108) we L(P ) = Q obtain f [w] = κ(w(x)). That is, the distortion functional (7.108) corresponds to the deformation function κ. Inserting this result into (7.117) and changing the order of the integrations, we obtain ⎤ ⎡ t

κ(P ) ∂P ⎦ I[P, Pst ] = . (7.140) dx ⎣ dt ln κ(P ∂t st ) Ω Since κ(z) is a function of z, the integral (7.140) can be written as ⎤ ⎡ P

(x)

κ(z) ⎥ ⎢ I[P, Pst ] = dz ln dx ⎣ ⎦ . κ(P (x)) st Ω

(7.141)

Using the entropy measure

Sκ [P ] = −

dx

P

dz ln κ(z)

(7.142)

Ω

and taking into account that stationary distributions satisfy ln[κ(Pst )] = x −V (x)/Q with V (x) = − h(x ) dx (see (7.139)), we can write I as I = −Sκ [P ] +

1 V (X) . Q

(7.143)

The functional I is a good candidate for a Lyapunov functional. By means of the explicit expression for I, we can now examine whether or not I is bounded from below. Furthermore, we arrive once again at an interpretation of I in terms of a free energy measure, F = QI = V − Q Sκ [P ], and we see that (7.139) is a free energy Fokker–Planck equation (4.4) for F .

324


Equation (7.60) Discussed in Sect. 7.2.2 Let us consider (7.60) as a special case of (7.101). Comparing (7.60) and (7.101), we obtain M = 1, h(x) + k[x, P ] = −dδU/δP dx, and L(P ) = QD2 (P )P . Let us put h(x) = −dδUL /δP dx = −dU0 /dx and k[x, P ] = −dδUNL /δP dx. Then, (7.122) and (7.123) read UL + INL [P ] , Q

d ∂P d UNL + dx INL [P ] = ∂t dt dt Q Ω I[P ] =

x

(7.144) ∂ 1 D (P )P . dx P (x , t; u) ∂x 2 Y

(7.145) The integral Y can be transformed into 6 7

P ∂P D2 (z) D2 (P ) + Y = dx dz ∂t z Ω

P D (z) d = dxP dz 2 . z dt Ω

(7.146)

Introducing the entropy

S[P ] = S0 −

P (x)

Ω

P (x)

D2 (z) dz dx , z

(7.147)

we can write the functional INL as INL = UNL /Q − S, which implies that F = QI is given by F = U − QS. That is, we have reobtained the free energy and entropy measures derived in Sect. 7.2.2.

7.3 Examples 7.3.1 Traveling Waves In Sect. 5.3.2, the KSS model was studied from the perspective of free energy Fokker–Planck equations. In general, the KSS model is defined by the nonlinear Fokker–Planck equation

∂ ∂ ∂ ∂2 P (x, t; u) = − ω− UMF (x − x )P (x , t; u) dx P + Q 2 P , ∂t ∂x ∂x Ω ∂x (7.148) for a random variable X ∈ [0, 2π] and t ≥ t0 . Here, UMF (z) describes an arbitrary coupling potential with a Fourier expansion given by

7.3 Examples

UMF (z) = −

∞

[cn cos(nz) + cn sin(nz)]

325

(7.149)

n=1

and cn , cn ∈ lR. Just as in Sect. 5.3.2, we have put a minus sign in (7.149), which implies that for cn > 0 and cn = 0 the potential UMF (z) has a minimum at z = 0. Note also that the very first Fourier coefficient, which describes a constant offset, has been neglected because the corresponding term in the Fokker–Planck equation vanishes (i.e., for UMF = c0 we have c0 ∂ Ω P (x , t; u) dx ]/∂x = 0). By means of the moving frame transformation (7.56), (7.150) P (y, t) = P (y + ω(t − t0 ), t; u) , we transform (7.148) into

∂ ∂2 ∂ dUMF (y − y ) P (y, t) = P (y, t) P (y , t) dy + Q 2 P (y, t) , dy ∂y ∂t ∂y Ω (7.151) and, in doing so, eliminate the constant drift force described by ω. Stationary solutions It is clear that the uniform distributions Pst (x) =

1 1 , Pst (y) = 2π 2π

(7.152)

are stationary solutions of (7.148) and (7.151). With respect to the moving frame, further stationary distributions satisfy U (y − y )Pst (y ) dy Ω MF − 1 Q Pst (y) = e , (7.153) Z which can be verified by substituting (7.153) into (7.151), see also (5.213). Note that the implicit equation (7.153) is also solved by the uniform distribution Pst (y) = 1/(2π) for Z = 1/(2π). Whereas the uniform stationary distribution exists for all coupling potentials UMF and parameters ω and Q, nonuniform stationary distributions of the form (7.153) do not necessarily exist. If a nonuniform stationary distribution exists, then there exist infinitely many of them due to the invariance of the system with respect to shifts of the phase space. That is, if Pst (y) = 1/(2π) is a stationary solution, then Pst (y + ∆y) for arbitrary ∆y is a stationary solution as well. Traveling Wave Solutions If nonuniform stationary distributions (7.153) exist, then they give rise to traveling wave solutions. Traveling wave solutions are solutions P (x, t; u) that

326


exhibit a fixed overall shape, but this shape is shifted with time along the xaxis, see Fig. 7.1. From (7.150) it follows that P (x, t; u) = P (x − ω(t − t0 ), t). Using (7.153) and the inverse transformation of (7.150) given by Pst (x, t; u) = Pst (x − ω(t − t0 )) ,

(7.154)

we conclude that traveling wave solutions of (7.148) are described by UMF (x − ω(t − t0 ) − y )Pst (y ) dy − Ω 1 Q , (7.155) Pst (x, t; Pst ) = e Z where u(x) is given by Pst (x) (i.e., we have Pst (x, t0 ; Pst ) = Pst (x)). The moving frame transformation (7.150) can be exploited to draw further conclusions. If an H-theorem holds for the moving frame system, that is, if P (y, t) → Pst (y) for t → ∞ holds, then the solutions of (7.148) either converge to the uniform distribution or to traveling wave solutions (7.155). – If the uniform stationary distribution in the moving frame is asymptotically stable (unstable), then the uniform stationary distribution in the fixed frame is asymptotically stable (unstable) as well. – If a nonuniform stationary distribution Pst (y) in the moving frame is stable (unstable), then the corresponding traveling wave solutions (7.155) are stable (unstable). Here, stable means that for all kinds of initial distributions u(x) = Pst (x) + (x), where (x) describes a small perturbation, the solution Pst (x, t; u) converges to a traveling wave solution Pst (x, t; u ) = Pst (x − ω(t − t0 ) − ∆x) that has the same shape as the unperturbed solution but in general differs with respect to the phase offset (i.e, we have u (x) = Pst (x − ∆x)).

–

0.3 0.25 P(x) 0.2 0.15 0.1 0.05 0

1

2

3 x

4

5

6

Fig. 7.1. Illustration of a traveling wave solution of (7.148)

7.3 Examples

327

General Case In general, the coupling potential UMF exhibits nonvanishing Fourier coefficients cn . Let us examine the stability of the uniform stationary distribution in this case by means of linear stability analysis [365]. We put P (y, t) = Pst (y) + (y, t) =

1 + (y, t) , 2π

(7.156)

where denotes a small perturbation. Substituting (7.156) into (7.151) and taking only terms linear in into account, we obtain

∂ ∂2 1 ∂2 U (y − y )(y , t) dy + Q (y, t) . (7.157) (y, t) = MF ∂t 2π ∂y 2 Ω ∂y 2 The Fokker–Planck operator Fˆ defined by ∂2 Fˆ (y, t) = Q 2 (y, t) ∂y

(7.158)

√ has complex valued eigenfunctions given by n (y) = exp{iny}/ 2π that 2 n /∂y 2 = −n2 n . Consequently, we express (x, satisfy ∂ √ t) in terms of ∞ (y, t) = −∞ an (t) exp{iny}/ 2π with a0 = 0 because of Ω (y, t) dy = 0. Note that the coefficients an satisfy an = a∗−n (where a∗−n denotes the complex conjugate of a−n ). Likewise, ∞ we describe UMF by means of the Fourier expansion UMF (z) = − n=−∞ cñ exp{inz}/2 with complex coefficients cñ = cn + icn . Then, we get

1 iyn UMF (y − y )(y , t) dy = − √ cñ e ak e−iy n eiy k dy 2 2π n Ω k Ω 2πδnk π = −√ cñ an eiyn (7.159) 2π n and ∂ 1 ∂2 cñ (y, t) = √ an (t)eiyn Q − 2 ∂t 2π ∂y 2 n cñ 1 n2 an (t)eiyn . Q− = −√ 2 2π n

(7.160)

√ ∞ Substituting (y, t) = −∞ an (t) exp{iny}/ 2π into (7.160) and exploiting the orthogonality of the eigenfunctions, we finally obtain d cñ 2 an (t) . an (t) = −n Q − (7.161) 2 dt

328


From (7.161) it follows that for Q − Re(˜ cn )/2 > 0 the Fourier amplitudes an (t) vanish and Pst = 1/(2π) is asymptotically stable. In contrast, if there is an index n such that Q − Re(˜ cn )/2 < 0, then the amplitude an (t) increases as a function of time and Pst = 1/(2π) is unstable. In sum, the stability of the uniform distribution is determined by the signs of the coefficients ˜ n = Q − cn , λ 2

(7.162)

where cn describe the real part of cñ . Nonstationary Solutions and Traveling Wave Solutions The previously derived result carries over to the stationary solution Pst (x) = 1/(2π) of (7.148): Pst (x) = 1/(2π) is asymptotically stable if the inequality ˜ n > 0 holds for all n and unstable if there is at least one λ ˜ n with λ ˜ n < 0. λ As a result, if the uniform distribution becomes unstable, it might be the case that the nonlinear Fokker–Planck equation (7.148) has only solutions that are nonstationary in the limit t → ∞. The shape of these nonstationary solutions may vary with time. However, if P (y, t) converges to a nonuniform stationary probability density Pst (y) in the limit t → ∞, then P (x, t; u) converges to a traveling wave solution described by P (x, t; Pst ) = Pst (x − ω(t − t0 )). Unfortunately, at this stage we cannot determine the asymptotic behavior of P (y, t), which implies that we cannot determine whether or not P (x, t; u) converges to traveling wave solutions if the uniform distribution becomes unstable. Free Energy Case with ω = 0 If cn = 0 holds for every n, then UMF defined by (7.149) corresponds to a symmetric potential. In this case, (7.151) is equivalent to the KSS model discussed in Sect. 5.3.2. That is, with respect to the moving frame we are dealing with a free energy Fokker–Planck equation. For this Fokker–Planck equation the H-theorem of free energy Fokker–Planck equations applies and, consequently, the limiting case ∂P /∂t = 0 for t → ∞ holds. This, in turn, implies that the limiting case lim P (x, t; u) = P (x, t; Pst ) = Pst (x − ω(t − t0 ))

t→∞

(7.163)

holds. Equation (7.163) states that transient solutions of (7.148) converge either to traveling wave solutions (if Pst differs from the uniform distribution) or to the uniform distribution (if Pst corresponds to the uniform distribution). Furthermore, from the stability analysis carried out in Sect. 5.3.2, we conclude ˜ = Q − cn /2 > 0 holds for all n, then P = 1/(2π) and, consequently, that if λ st the uniform probability density Pst (x) = 1/(2π) is asymptotically stable. If ˜ = Q − cn /2 < 0, then P (y) = 1/(2π) there is at least one index n with λ st

7.3 Examples

unstable stationary uniform distribution

329

stable stationary uniform distribution λn

stable traveling waves 0

Fig. 7.2. Bifurcation diagram for solutions of (7.148) for symmetric potentials UMF (z). Traveling wave solutions emerge from the uniform distribution when coef˜ n become negative ficients λ

as well as Pst (x) = 1/(2π) are unstable (see also (5.227)). Note that this result is consistent with the stability analysis derived for the general case (see (7.162)). Taking the implications of the H-theorem and the stability analysis together, we obtain a clear picture about the behavior of the uniform distribution at an instability point, see Fig. 7.2. If the distributions Pst (x) = Pst (y) = 1/(2π) become unstable due to a change of the control parameters, then P (y, t) converges to a stable nonuniform distribution and P (x, t; u) approaches a stable traveling wave solution of the form (7.155). Finally, note that in the parameter regime with the stable uniform distribution we do not have traveling wave solutions if we deal with a sine coupling-force, because in this case the uniform distribution is the only possible stationary solution (see Sect. 5.3.2). 7.3.2 Reentrant Noise-Induced Phase Transitions Reentrant phase transitions have bifurcation lines that are qualitatively different from the bifurcation line shown in Fig. 5.18 [601]. For example, a system with a monostable and a bistable parameter regime and a control parameter α ∈ [0, ∞) exhibits a reentrant phase transition if it is bistable for a control parameter α ∈ [c1 , c2 ] and monostable for α ∈ [c1 , c2 ] with 0 < c1 < c2 < ∞. In this case, by increasing gradually the control parameter α we enter the bistable regime at α = c1 and leave the bistable regime at α = c2 . For examples, see [219, 224, 434, 466, 601, 602]. In this section we will study a reentrant phase transition, which arises due the impact of a multiplicative noise source that, in turn, induces a drift term via the Stratonovich interpretation [187]. To this end, we return to our discussion in Sect. 7.2.3 and consider a system described by the nonlinear Fokker–Planck equation (7.91) and the matching condition (7.81). We choose the drift and diffusion coefficients in line with coefficients that have frequently been used in the context of √ reentrant bifurcations [219, 224, 434, 466, 601, 602]. We use g(x) = Q (1 + bx2 ) and D2 (x) = Q(1 + bx2 )2 with b > 0, which means that there is a mean field force

330


√ √ x involving A(x) = c 0 D2−1 (x ) dx = c[arctan( bx)/ b + x/(1 + bx2 )]/(2Q). Since the expression arctan(x) + x/(1 + x2 ) behaves like an arctan-function1 , we introduce the modified arctan-function x arctan (x) = arctan(x) + . (7.164) 1 + x2 For c = 2Q we then obtain from (7.91) the mean field model 6 B C7 √ √ ∂ arctan ( bx) ∂ arctan ( bX) √ √ P (x, t; u) = − h(x) − κ − P ∂t ∂x b b +Q

∂ ∂ 1 + bx2 1 + bx2 P . ∂x ∂x

(7.165)

Furthermore, we put h(x) = −ax(1 + bx2 )2 with a > 0 [601]. then, stationary distributions of (7.165) satisfy the implicit equation Pst (x) =

⎧ ⎛ 6 B C 7 2 ⎞⎫ √ √ ⎬ ⎨ 1 arctan ( bX) 1 ⎝ 2 κ arctan ( bx) ⎠ √ √ ax + − exp − 2 ⎭ ⎩ 2Q 2 Z(1 + bx ) b b st

√

(7.166)

(see (7.94) and replace Z Q by Z). Accordingly, the self-consistency equation m = R(m) for m = arctan (X) involves the functions ⎧ ⎛ 6 72 ⎞⎫ √ ⎬ ⎨ 1 1 1 ⎝ 2 κ arctan ( bx) ⎠ , √ P (x, m) = ax + exp − − m ⎭ ⎩ 2Q 2 Z(m) 1 + bx2 b

arctan (x)P (x, m) dx . (7.167) R(m) = Ω

Symmetric Solution Since arctan (x) describes an antisymmetric function, the relation R(0) = 0 holds, which in turnE implies that a symmetric solution Pst with X = 0 and D √ √ arctan ( bX)/ b = 0 exists for all parameters κ and Q. Note that for stationary distributions of the form (7.166), the implication Xst = 0 ⇔ D √ √ E arctan ( bX)/ b = 0 holds. st

Asymmetric Solutions and Reentrant Phase Transitions Let us examine the emergence of asymmetric solutions with nonvanishing first moments. To this end, we first determine the qualitative behavior of 1

Both arctan(x) and arctan(x) + x/(1 + x2 ) are symmetric and bounded functions that increase strictly monotonically: d[arctan(x)+x/(1+x2 )]/dx = 2/(1+x2 )2 > 0.

7.3 Examples

331

R (m) = R(m) − m. It is clear that the relation R (m) = 0 defines solutions of the self-consistency equation m = R(m). Moreover, if the inequality dR (m)/dm < 0 (> 0) holds for R (m) = 0, we are dealing with solutions of m = R(m) with dR/dm < 1 (> 1) and asymptotically stable (unstable) stationary distributions (see Sect. 7.2.3). The function R (m) is shown in Fig. 7.3 values E √ of Q. We realize that when asymmetric solutions D for three √ with arctan ( bX) / b = 0 and X = 0 emerge, then the symmetric solution becomes unstable (because the slope dR (0)/dm becomes positive). In addition, we see that the bifurcation is reentrant. Bifurcation lines can ˜ = 0 ⇒ dR(m)/dm = κKA,st /c = 1 with c = 2Q (see be computed from λ Sect. 7.2.3) and are depicted in Fig. 7.4. The bifurcation diagram for the order parameter m = Ast as a function of Q is given in Fig. 7.5. Note that in Fig. 7.5 only the stable solutions are shown. Assuming that (7.165) describes a strongly nonlinear Fokker–Planck equation we have determined the stationary solutions of (7.165) by solving numerically the corresponding Ito–Langevin equation, see Fig. 7.5. In line with (7.92), this Ito–Langevin equation reads D E2 √ √ d κ 1 X(t) = h(X) − √ arctan ( bX) − arctan ( bX) dt b dg(X) +g(X) + g(X)Γ (t) , (7.168) dx 2 2 with drift √ and diffusion functions given by h(x) = −ax(1 + bx ) and g(x) = Q(1 + bx2 ) (see above). Finally, note that the reentrant phase transitions discussed here may describe the emergence and the vanishing of group behavior in populations of interacting members as argued in Sect. 5.5.5.

R’(m)

0.4 0.3 0.2

Q=10.0

0.1 –3

–2

–1

0 –0.1

1

Q=1

2

m

3

–0.2 –0.3

Q=40

–0.4

Fig. 7.3. Illustration of the self-consistency equation R (m) = R(m)−m = 0 for the nonlinear Fokker–Planck equation (7.165). The function R (m) for κ = 20 and a = 1 is depicted for several values of Q: Q = 1, Q = 10, Q = 40. Solutions of R (m) = 0 describe stationary distributions. Solutions of R (m) = 0 with negative (positive) slopes correspond to asymptotically stable (unstable) distributions; reprinted from c 2004, with permission from Elsevier [187],

332

7 General Nonlinear Fokker–Planck Equations κ

20

<X> =/ 0

15 k

10

<X> = 0

5

0

10

5

15

20 Q

25

30

35

Fig. 7.4. Bifurcation lines of reentrant phase transitions described by the mean field model (7.165). Bifurcation lines are computed from κKA,st /(2Q) = 1 for a = 1 (solid line) and a = 1.5 (thick dashed line) and for b = 0.2; reprinted from [187], c 2004, with permission from Elsevier 2

m

1

0

10

20

30

40

50

Q –1

–2

√ √ Fig. 7.5. Order parameter m = arctan ( bX)/ b st of a reentrant bifurcation described by (7.165). Solid lines are computed from m = R(m) and (7.167). Crosses and diamonds are obtained from simulations of Langevin (7.168) using the averaging method for self-consistent Langevin equations. The noise amplitude Q is gradually increased along the horizontal line depicted in Fig. 7.4. Parameters: a = 1, b = 0.2, κ = 20 (L = 20000, ∆t = 10−4 , wn via Box–Muller. The control parameter Q is gradually increased starting with Q = 1. For every Q value 2 × 105 iterations were carried out. Random variables for upper and lower branches are initially delta c 2004, with permission from distributed at 0.01 and −0.01); reprinted from [187], Elsevier 7.3.3 Systems with Multistable Variability So far, we have primarily discussed Fokker–Planck equations that either exhibit finite dimensional nonlinearities and are nonlinear with respect to their drift terms (see Chap. 5), or exhibit infinite dimensional nonlinearities and are nonlinear with respect to their diffusion terms (see Chap. 6). In contrast, we consider now the Fokker–Planck equation ∂ ∂ ∂2 P (x, t; u) = γxP + D2 (A(X))P ∂t ∂x ∂x2

(7.169)

7.3 Examples

333

that is nonlinear with respect to the diffusion term and features a diffusion coefficient that depends on a single order parameter A [194]. We assume that γ > 0 and X ∈ Ω = lR and consider solutions P subjected to natural boundary conditions. Note that D2 does not depend explicitly on x. Therefore, the diffusion term can also be written as D2 (A(X))∂ 2 P/∂x2 . Furthermore, we require D2 (z) > 0. Substituting D1 (x) = −γx and D2 (x, A) = D2 (A) into (7.4), we obtain 0 γx2 γ exp − . (7.170) Pst (x) = 2πD2 (Ast ) 2D2 (Ast ) Note that we have determined the normalization constant of (7.170) by means of the Gaussian distribution (3.110). In a similar vein, from (7.6) and (7.7) it follows that 0 γ γx2 P (x, m) = (7.171) exp − 2πD2 (m) 2D2 (m)

and R(m) =

A(x)P (x, m) dx ,

(7.172)

Ω

which gives us the self-consistency equation m = R(m). The stationary order parameter values Ast that satisfy (7.170) correspond to the solutions m of the self-consistency equation m = R(m). Alternatively, we may determine Ast in a two-step approach. Accordingly, the first step is to determine D2 (Ast ). To this end, we note that the relation

0 γ γx2 dx (7.173) D2 (Ast ) = D2 A(x) exp − 2πD2 (Ast ) 2D2 (Ast ) Ω holds. Therefore, we define 0

γ γx2 , exp − 2πm 2m

˜ ˜ A(x)P (x, m) dx , R(m) = D2

P˜ (x, m) =

(7.174) (7.175)

Ω

and the self-consistency equation ˜ m = R(m) .

(7.176)

Solutions of (7.176) give us the stationary parameters values D(Ast ). In a second step, we substitute D(Ast ) into (7.170) and compute Ast = A(x)Pst (x) dx. Ω In order to determine the stability of the distribution (7.170), one may examine the stability of cumulants M1 and K. Multiplying (7.169) by x and

334


x2 , respectively, integrating with respect to x, and using partial integration, we obtain the evolution equations d M1 (t) = −γM1 (t) dt

(7.177)

and

d M2 (t) = −2γM2 (t) + 2D2 (A) . (7.178) dt In deriving these results, we have assumed that the surface terms vanish that arise from the integrations by parts. It is clear from (7.177) and (7.178) that the variance K = M2 − (M1 )2 evolves like d K(t) = −2γK(t) + 2D2 (A) . dt

(7.179)

From (7.177) we read off that the first cumulant M1 is asymptotically stable and vanishes in the long time limit, which is consistent with (7.170). Therefore, at issue is to study the evolution of K(t). To this end, we first derive an exact time-dependent solution of (7.169). Substituting PG (x, t; u) = for u =

− 1 e 2πK(t)

[x − x0 M1 (t)]2 2K(t)

(7.180)

−1 2πK(t0 ) exp{−[x − x0 ]2 /2K(t0 )} into (7.169), we obtain d M1 (t) = −γM1 (t) , dt d K(t) = −2γK(t) + 2D2 (APG ) . dt

(7.181)

By means of this time-dependent solution, we can study the behavior of perturbations of the stationary variance Kst = D2 (Ast ). To this end, we consider the initial distributions u(x) =

1 2π(Kst + v0 )

[x − w0 ]2 − e 2(Kst + v0 ) ,

(7.182)

where v0 and w0 denote small quantities. For M1 (t) = M1 (t0 ) + w(t) = w(t) and K(t) = Kst + v(t) with w(t0 ) = w0 and v(t0 ) = v0 , the distribution (7.180) and the evolution equations (7.181) become PG (x, w(t), v(t)) =

[x − w(t)]2 − 1 e 2[Kst + v(t)] 2π[Kst + v(t)]

(7.183)

7.3 Examples

335

and d w(t) = −γw(t) , dt d v(t) = −2γ(v(t) + Kst ) + 2D2 (APG (x,w,v) ) . dt

(7.184) (7.185)

From (7.184) it follows that perturbations w vanish in any case. In order to gain some insight into the evolution of v(t), we consider an interval I = [t0 , t0 + ∆t] for which v(t) and w(t) with t ∈ I can be regarded as small quantities and linearize (7.185) with respect to v and w. Accordingly, we find

∂ APG (x,w,v) = Ast + A(x)PG (x, w, v) dx v ∂v Ω v=w=0

∂ + A(x)PG (x, w, v) dx w + O(vw, v 2 , w2 ) . (7.186) ∂w Ω v=w=0 Y

In what follows, we assume that A(x) = A(−x) holds. Then, we have Y = 0 and, taking only linear terms into account, (7.186) becomes

∂ APG (x,w,v) = Ast + A(x)PG (x, w, v) dx v, (7.187) ∂v Ω v=w=0 which implies that 9 : D2 APG (x,w,v) = D2 (Ast )

dD2 (z) ∂ + A(x)PG (x, w, v) dx v. dz ∂v Ω z=A v=w=0

(7.188)

st

Note that in (7.188) we have again taken into account only terms that are linear in v. Using −2γKst + 2D2 (Ast ) = 0, from (7.185) and (7.188) we finally obtain 7 6

∂ d dD2 (z) 2v . A(x)PG (x, w, v) dx v(t) = − γ − dt dz z=A ∂v Ω v=w=0 st

(7.189) Let us define the stability coefficient

dD2 (z) ∂ ˜ λ=γ− A(x)PG (x, w, v) dx . dz ∂v Ω z=A v=w=0

(7.190)

st

˜ < 0 the variance is unstable, which implies that Pst is unstable. For For λ ˜ λ > 0 the variance is asymptotically stable, which is a necessary condition for

336


Pst being asymptotically stable. As we will show next, there is a geometrical ˜ Using interpretation of λ.

∂ ∂ A(x)PG (x, w, v) dx =γ A(x)P˜ (x, m) dx ∂v Ω ∂m Ω v=w=0 D2 (Ast ) (7.191) and

˜ dR d dD2 (z) ˜ (x, m) dx = A(x) P , (7.192) dm dz dm Ω z=A D2 (A ) Ast

we get

st

st

⎤

⎡

˜ d d R(m) v(t) = −2γ ⎣1 − dt dm ˜ dR(m) ˜ λ=1− dm

and

⎦v

(7.193)

D2 (Ast )

.

(7.194)

D2 (Ast )

˜ is related to the slope of R(m) ˜ ˜ That is, λ at intersection points m = R(m). Therefore, the linear stability analysis that we have carried out above is consistent with a stability analysis based on the self-consistency equation (7.176). H-Theorem We consider now a diffusion coefficient D2 (A) for which the Gaussian solution (7.180) converges to its stationary solution (7.170) in the long time limit. As we will show next, in this case, transient solutions in general converge to stationary ones [194]. Let us consider the solution W (x, t; u) of the linear Fokker–Planck equation ∂ ∂2 ∂ W (x, t; u ) = γxW (x, t) + 2 D2 (A(X)P )W , (7.195) ∂t ∂x ∂x where A(X)P = Ω A(x)P (x, t; u) dx is the expectation value related to a solution of the nonlinear Fokker–Planck equation (7.169). We consider the initial distribution 2 1 [x − µ(t0 )] , (7.196) u (x) = exp − 2(t0 ) 2π(t) with µ(t0 ) = XP (x,t0 ;u) ,

(t0 ) = [x − µ(t0 )]2 P (x,t

0 ;u)

.

(7.197)

7.3 Examples

Then, by analogy to (7.180) and (7.181) we realize that 2 1 [x − µ(t)] W (x, t; u ) = exp − 2(t) 2π(t)

337

(7.198)

is a solution of (7.195) for d µ(t) = −γµ , dt d (t) = −2 γ + 2D2 (AP ) . dt

(7.199)

In general, the initial distribution u(x) of P does not correspond to u (x) of W and, consequently, the distributions W and P are not equivalent. Next, we exploit the H-theorem for linear Fokker–Planck equations [498]. We use the Boltzmann–Kullback measure

P (x, t; u) B dx ≥ 0 , (7.200) K[P, W ] = P (x, t; u) ln W (x, t; u ) Ω see (4.123). The key issue for the proof of the H-theorem is to realize that by definition the evolution equations for W and P have common drift and diffusion coefficients. In particular, the diffusion coefficient D2 describes for both evolution equations the same time-dependent function D2 (t) = D2 (A). On account of this property, we can calculate the derivative of K by means of standard techniques developed for linear Fokker–Planck equations [498] and thus obtain 2

d B ∂ P (x, t; u) K[P, W ] = −2D2 (A) P (x, t; u) dx ≤ 0 . ln dt ∂x W (x, t; u ) Ω (7.201) From (7.200) and (7.201) it follows that in the limit t → ∞ the derivative of K vanishes. From D2 > 0 and limt→∞ dK/ dt = 0 it follows that lim [P (x, t; u) − W (x, t; u )] = 0 .

t→∞

(7.202)

Equation (7.202) implies that in the limit t → ∞ the expectation values A of P (x, t; u) and W (x, t; u ) become equivalent: limt→∞ [AP − AW ] = 0. For AP = AW the distribution W corresponds to the Gaussian solution PG described by (7.180). Consequently, we obtain P (x, t; u) = W (x, t; u ) = PG (x, t; u )

(7.203)

for t → ∞. For diffusion coefficients D2 , for which PG converges in the limit t → ∞ to a stationary solution of the form (7.170), we conclude that for arbitrary initial distributions u(x) the general solution P (x, t; u) converges to a stationary distribution of the form (7.170).

338


Pitchfork Bifurcation Model As an example, we will study a many-body system with a diffusion coefficient D2 that is composed of two parts: D2 = Q + QMF . Here, Q corresponds to a constant fluctuation strength, whereas QMF couples the subsystems. For QMF = 0 the stationary second moment M2,st is given by M2,st = Q/γ. We assume that QMF measures the deviation of the second moment M2 (t) from Q/γ. We choose 2 Q 3

2 Q −β X − , (7.204) X − D2 X 2 = Q + α γ γ with α > 0 and β > 0. Substituting D2 into (7.169), we get 2 Q 3 2 Q ∂ ∂ −β P (x, t; u) = γ xP + Q + α X − X − γ γ ∂t ∂x

∂2 P. ∂x2 (7.205) An evolution equation for M2 can be obtained by multiplying (7.205) with x2 , integrating with respect to x, and integrating by parts: 3 d Q Q M2 (t) = −2(γ − α) M2 (t) − − 2β M2 (t) − . (7.206) dt γ γ Equation (7.206) describes a pitchfork bifurcation of the variable q(t) = (a) M2 (t) − Q/ γ [246, 255, 448]. The stationary values become M2,st = Q/ γ (b,±) for α > 0 and M2,st = Q/ γ ± (α − γ)/ β for α > γ, see Fig. 7.6. Using (a)

conventional linear stability analysis, we find that M2,st describes an asymptotically stable stationary solution of (7.206) for α < γ and an unstable one M2 2.0 1.5 1.0 0.5

1.0

2.0

3.0

4.0

5.0

6.0

ε

Fig. 7.6. Bifurcation diagram: M2,st as function of = α/γ (stable solutions only). Both curves were computed from the Langevin equation (7.210) using the averaging method for self-consistent Langevin equations. Parameters: γ = Q = 1, β = 4 (L = 104 , ∆t = 0.01, 3000 iterations for every , wn via Box–Muller) [194]

7.3 Examples

339

(b,±)

for α > γ, whereas M2,st describe stable stationary solutions for α > γ. The stability of M2 may carry over to the stability of the corresponding stationary probability densities. In fact, we obtain the very same results from the stability analysis based on (7.189) and (7.190). To see this, we substitute (7.204) with dD2 (z)/dz = α + 3β(z − Q/γ)2 and Ω A(x)PG (x, w, v) dx = M2,st + v ˜ = γ − α for M (a) . Likewise, for for w = 0 into (7.190) and thus obtain λ 2,st (b,±) ˜ = −2(γ − α). These results indicate that for α < γ (i.e. for M we get λ 2,st

(a)

= α/γ < 1) the stationary probability density (7.170) with Ast = M2,st is stable, whereas for α > γ (i.e. for = α/γ > 1) it is unstable and there (b,±) are two stable stationary probability densities (7.170) with Ast = M2,st . In fact, numerical simulations confirm this hypothesis, see Figs. 7.6 and 7.7.

0

0 1

2

0.4

P(x) 0.2

4

0

ε

0.8

P(x) 0.4

2

0 -4

-2

0

6

x

2

4

-4

ε

3 -2

0

x

2

4

Fig. 7.7. Left: stationary stable probability densities corresponding to the upper branch in Fig. 7.6. Beyond the critical value = 1 the probability density evolves towards the uniform distribution when is increased. Right: stationary stable probability densities corresponding to the lower branch in Fig. 7.6. Beyond the critical value = 1 the probability density evolves towards a δ-distribution for increasing [194]

Basins of Attraction We consider the bistable regime with α > γ. Equation (7.206) can be written as d dV M2 (t) = − , (7.207) dt dM2 with 2 4 Q β Q z− + . (7.208) V (z) = (γ − α) z − γ 2 γ From (7.208) we see that the potential V is bistable and symmetric with respect to z0 = Q/γ (i.e., we have V (Q/γ + z) = V (Q/γ − z)). Therefore,

340


for initial distributions u(x) with M2 (t0 ) > Q/γ the second moment converges to the potential minimum at z > Q/γ, which implies that P (x, t; u) (b,+) converges to the Gaussian stationary distribution (7.170) with M2,st = Q/γ + (α − γ)/β. In contrast, for initial distributions with M2 (t0 ) < Q/γ we find that M2 (t) converges to the potential minimum at z < Q/γ, which (b,−) implies that P (x, t; u) converges to Pst with M2,st = Q/γ − (α − γ)/β, see Fig. 7.8. We conclude that there are two basins of attraction in the function space of probability densities. These basins are separated by initial distributions u(x) with vanishing second moment. For these initial distributions solu(a) tions P (x, t; u) converge to the unstable stationary solution with Mst = Q/γ. That is, initial distributions u(x) with M2 (t0 ) = 0 describe a separatrix in the function space of probability densities that separates the basins of attraction.

1.6 1.4 1.2 M2 1 0.8 0.6 0.4 0

0.2

0.4

0.6

0.8

1

1.2

t

1.4

Fig. 7.8. Order parameter M2 as a function of t as obtained from a simulation of the Langevin equation (7.210) using the averaging method (diamonds) and from solving numerically (7.207) (solid lines) for initial distribution u(x) with different M2 (0) (t0 = 0). The initial distributions were symmetric uniform distributions u(x) = 1/(2a) for x ∈ [−a, a] and u(x) = 0 for x ∈ [a, a]. We considered the bistable regime = α/γ > 1. For initial distributions with M2 (0) > Q/γ stochastic processes converge to the wide stationary solution with M2,st > Q/γ (dashed upper line). For initial distributions with M2 (0) < Q/γ stochastic processes converge to the narrow stationary solution with M2,st < Q/γ (dashed lower line). Initial values: M2 (0) = 1.7, M2 (0) = 1.1, M2 (0) = 0.9, and M2 (0) = 0.25 (from top to bottom). Parameters: Q = 1, γ = 1, α = 2, β = 4 (L = 5 × 105 , ∆t = 0.01, wn via Box–Muller)

7.4 Applications

341

Langevin Equation For every initial distribution u(x) the second moment M2 defined by (7.207) corresponds to a function of time which describes the overdamped motion of a particle in the globally attractive potential (7.208). Consequently, by substituting M2 (t, u) as a function of t into (7.205), we can write (7.205) as a linear Fokker–Planck equation involving a diffusion coefficient D2 (t, u) that depends on time t and the initial distribution u. We consider now only initial distributions u(x) with second moments M2 (t0 , u), for which the inequalities M2 (t, u) > 0 , D2 (t, u) > 0

(7.209)

hold, where M2 (t, u) is the solution of (7.207). Then, the linear Fokker–Planck equation related to D2 (t, u) is well-defined, which implies that (7.205) is a strongly nonlinear Fokker–Planck equation (see Chap. 3) that can be studied numerically by means of its corresponding Ito–Langevin equation. Introducing the control parameter = α/γ, the Ito–Langevin equation of (7.205) reads 3 d Q Q X(t) = −γX(t) + Q + γ X 2 − − β X 2 − Γ (t) . dt γ γ (7.210) From our previous discussion of (7.206) it follows that the pitchfork bifurcation occurs if α = γ holds, which means that the critical point is at = 1. (a) Note that D2 > 0 is always satisfied by the stationary values M2,st and (b,+)

(b,−)

M2,st . However, the admissible range of is restricted in the case of M2,st . (b,−)

Substituting M2,st into (7.204), we see that the requirement D2 > 0 implies that must satisfy < Q2 β/γ 3 + 1. Figure 7.6 shows the bifurcation diagram (b,−) obtained by simulating (7.210). The simulation of the lower branch (M2,st ) indicates the convergence of the stationary probability density to a delta distribution when approaches its maximal admissible value max = Q2 β/γ 3 +1. In our simulation we have γ = Q = 1, β = 4, and max = 5. Figure 7.7 illustrates the stationary probability densities Pst (x) for different values of corresponding to the upper branch (left panel) and the lower branch (right panel) of the diagram in Fig. 7.6. Finally, Fig. 7.8 shows the evolution of the order parameter X 2 as computed from the Langevin equation (7.210) for several initial values and illustrates the basins of attraction of the two stationary solutions that exist for > 1.

7.4 Applications 7.4.1 Landau Form and Plasma Particles The evolution of the velocity distribution of plasma particles can be described by means of a nonlinear Fokker–Planck equation. Let us consider a plasma

342


composed of one species of charged particles. The particles are described by their positions and velocities. Considering a spatially homogeneous plasma, we are left with the density function for the particle velocities ρ(v, t) with v ∈ Ω = lR3 normalized to M0 = Ω ρ(v, t) d3 v. Alternatively, we may consider the probability distribution of particle velocities P = ρ/M0 . Then, P (v, t) satisfies the evolution equation 3 3 ∂ ∂2 ∂ P (v, t) = − Di (v, P )P + Dik (v, P )P , ∂vi ∂vi ∂vk ∂t i=1

(7.211)

i,k=1

with

P (v , t) 3 ∂ Di (v, P ) = a d v , ∂vi Ω |v − v |

∂2 |v − v | P (v , t) d3 v . Dik (v, P ) = b ∂vi vk Ω

(7.212)

Equation (7.211) is referred to as the Landau form of the Fokker–Planck equation [36, 85, 134, 138, 292, 347, 447]. The drift and diffusion terms involve the Rosenbluth potentials

P (v , t) 3 d v , Φ1 (v) = |v − v |

Ω |v − v | P (v , t) d3 v . (7.213) Φ2 (v) = Ω

The Landau form accounts for collisions of particles and Coulomb interactions between particles. Both transient solutions [13, 398, 447, 500, 560] and stationary solutions [540] have been studied. The Landau form can also be supplemented with additional drift terms related to the collisionless Boltzmann equation [52, 83, 84, 152]. Note that the Landau form of the Fokker– Planck equation also has applications in astrophysics [58, 370]. 7.4.2 Bunch-Particle Distributions of Particle Beams Particle beams of electron storage rings can be bunched. A particle bunch is a group of particles that move together and have roughly the same energy. Charged bunch-particles produce electromagnetic fields. These fields act back on the bunch-particles and are called wakefields [91, 628]. In line with the Vlasov theory for the interaction between charged particles and their fields, there is a mean field theory of the wakefields, which leads to Vlasov–Fokker– Planck equations for particle distributions [125, 126, 283, 284, 285, 286, 534, 535, 558, 609]. Our objective is to relate the solutions of these Fokker–Planck equations to the random motions of single beam particles [177].

7.4 Applications

343

Vlasov–Fokker–Planck Equations and Canonical-Dissipative Systems Let us describe the particles in bunched longitudinal beams traveling through electron storage rings in terms of their relative positions and rescaled energy deviations. Relative positions are defined with respect to moving frames related to the traveling bunches and will be denoted by q. Rescaled energy deviations will be denoted by p and are typically measured in terms of appropriately rescaled energy deviations from beam design energies. It then 2 turns out that the bunch-particle distribution ρ(p, q, t) with (p, q) ∈ Ω = lR and M0 = Ω ρ(p, q, t) dp dq satisfies the evolution equation ∂ ∂2 ∂ ∂ ∂H ∂ ∂H ρ = γ (pρ) + D 2 ρ , ρ(p, q, t) + ρ− ∂t ∂q ∂p ∂p ∂q ∂p ∂p

(7.214)

with H defined by

HW (q − q )ρ(p , q ) dp dq .

H = H0 (p, q) +

(7.215)

Ω

The first expression H0 (p, q) describes a single particle Hamiltonian and usually simply reads H0 (p, q) = p2 /2 + q 2 /2. The integral in (7.215) reflects particle-particle interactions in a self-consistent mean field fashion (Vlasov theory). The function HW determines the details of the wakefield that reflects the particle-particle couplings [125, 126, 283, 284, 285, 286, 534, 535, 558, 609]. The terms on the left-hand side of (7.214) describe damping and diffusion of the particles due to synchrotron radiation. Here, γ > 0 is a damping constant and D > 0 is a diffusion coefficient. The right-hand side of (7.214) is also called the Fokker–Planck collision operator. The left-hand side of (7.214) is of type of a Vlasov equation [85, 138, 347, 442, 447]. Therefore, we refer to (7.214) as a Vlasov–Fokker–Planck equation. Aiming at descriptions for single particle motions, we transform (7.214) into an evolution equation for a probability density P (p, q, t) = ρ(p, q, t)/M0 normalized to unity: ∂ ∂H ∂ ∂ ∂H ∂ ∂2 P− P (p, q, t) + P = γ pP + D 2 P , ∂p ∂p ∂q ∂p ∂p ∂q ∂t with

H = H0 (p, q) + M0

HW (q − q )P (p , q ) dp dq .

(7.216)

(7.217)

Ω

In general, HW (z) is composed of a symmetric and an antisymmetric part. If HW (z) describes a symmetric function, then there is a free energy approach to the problem at hand.

344


Langevin Equation Let us write (7.216) as ∂ ∂2 P (p, q, t) = −∇ · (hP ) + D 2 P , ∂p ∂t

(7.218)

with the probability-dependent drift vector

1 h(p, q, P ) = I(p, q, P ) + γp , 0

(7.219)

where I = (Ip , Iq ) is given by Ip = −∂H /∂q and Iq = ∂H /∂p and ∇ is defined by ∇ = (∂/∂p, ∂/∂q). We assume that for solutions of (7.218), the time-dependent drift vector h defined by h (p, q, t) = h(p, q, P ) corresponds to the first Kramers–Moyal coefficient of a Markov diffusion process. Then, (7.218) is a strongly nonlinear Fokker–Planck equation and the transition probability density P (p, q, t|p , q , t ) of the Markov diffusion process satisfies ∂ P (p, q, t|p , q , t) = ∂t −∇ · [h(p, q, P (p, q, t))P (p, q, t|p , q , t)] + D

∂2 P (p, q, t|p , q , t) , ∂p2 (7.220)

where P (p, q, t) is a solution of (7.218). Equations (7.218) and (7.220) define a Markov process in terms of the joint probability densities P (pn , qn , tn ; . . . ; p1 , q1 , t1 ) = P (pn , qn , tn |pn−1 , qn−1 , tn−1 ) · · · P (p2 , q2 , t2 |p1 , q1 , t1 )P (p1 , q1 , t1 ) , (7.221) see Chap. 3. Let p(t) and q(t) define the random variables related to P (p, q, t) = δ(p − p(t))δ(q − q(t)). Then, the joint probability densities (7.221) in general and P (p, q, t) in particular can also be obtained from the Langevin equation d ∂H0 (p, q) q(t) = , dt ∂p

∂ d ∂H0 (p, q) − M0 HW (q − q )P (p , q , t) dp dq p(t) = − dt ∂q ∂q Ω √ −γp + D Γ (t) . (7.222) Free Energy Case If HW (z) describes a symmetric function, then (7.216) can be interpreted as a free energy Fokker–Planck equation of a canonical-dissipative system. To see this, for HW (z) = HW (−z) we define the internal energy U [P ] as

7.4 Applications

U [P ] = H0 +

M0 2

Ω

345

HW (q − q )P (p, q)P (p , q ) dp dq dp dq . (7.223)

Ω

Furthermore, we define the conservative drift forces Ip = −

∂ δU , ∂q δP

Iq =

∂ δU ∂p δP

(7.224)

related to the conservative drift vector I = (Ip , Iq ). Using ∇ = (∂/∂p, ∂/∂q), the Vlasov–Fokker–Planck equation (7.216) can be written as ∂ ∂ δF ∂ P (p, q, t) = −∇ · (IP ) + γ P , ∂t ∂p ∂p δP

(7.225)

where F is the free energy F = U − Q BS involving the Boltzmann entropy S = − P ln P dp dq and a noise amplitude Q = D/γ. Equation (7.225) corresponds to a free energy Fokker–Planck equation of a canonical-dissipative system (see Sect. 4.6) and for H0 (p, q) = p2 /2 + q 2 /2 it can be regarded as a special case of the generalized Kramers equation (4.106) for systems with Boltzmann statistics. Consequently, stationary distributions can be obtained from the free energy principle δF/δP = µ. From (5.5) we obtain the implicit equation H (p, q, Pst ) 1 , (7.226) Pst (p, q) = exp − Q Z

B

with H given by (7.217). From solutions of (7.226) we then obtain the stationary particle density distributions ρst (p, q) = M0 Pst (p, q). Haissinski Distributions of Bunched Particle Beams Following [608], we confine ourselves to model the wakefield HW by means of a delta function: HMF = HW = κM0−1 δ(q − q ). In doing so, we will be able to derive analytical expressions and to study at least qualitatively possible impacts of wakefields. Then, for H0 (p, q) = p2 /2 + q 2 /2 the Vlasov–Fokker– Planck equation (7.216) reads ∂ ∂P (p, q, t) ∂P (p, q, t) ∂ P (p, q, t) + p − q + κ P (q, t) ∂t ∂q ∂p ∂q ∂ ∂2 =γ [pP (p, q, t)] + D 2 P (p, q, t) (7.227) ∂p ∂p and (7.222) becomes d q(t) = p , dt √ ∂P (q, t) d p(t) = −q − κ − γp + D Γ (t) , ∂q dt

(7.228)

346


with P (q, t) = P (p, q, t) dp = δ(q − q(t)). Stationary distributions can be found in the form of Pst (p, q) = Pst (p)Pst (q) with 1 p2 (7.229) exp − Pst (p) = √ 2Q 2πQ and Pst (q) given by [Q + κPst (q)]

dPst (q) = −qPst (q) . dq

(7.230)

This can be verified by substituting Pst (p, q) into (7.227) (see also [608]). Note also that we have Q = D/γ as stated earlier. Stationary solutions satisfying Pst (p, q) = Pst (p)Pst (q) with Pst (p) and Pst (q) described by (7.229) and (7.230) are called Haissinski solutions [91, 250]. Using a stability analysis similar to the one developed in Sect. 5.1, we can show that the Haissinski solutions are stable provided that they exist [608]. One may determine Pst (q) by solving the differential equation (7.230). Alternatively, from the free energy principle we obtain (7.226) in the form of 2 q /2 + κPst (q) 1 p2 Pst (p, q) = exp − exp − , (7.231) Z 2Q Q which gives us Pst (p, q) = Pst (p)Pst (q) as well as the distribution (7.229) and 2 1 q /2 + κPst (q) , (7.232) Pst (q) = exp − Z Q where Z is a normalization constant. Note that differentiating (7.232) with respect to q, we obtain (7.230) again. Equation (7.232) can be evaluated using the concept of distortion functions (see Sects. 4.7.1 and 7.2.4). To this end, we transform (7.232) into 1 1 κ q2 Pst (q) exp Pst (q) = W (q) , W (q) = √ , exp − Q Z 2Q 2πQ (7.233) where Z is another normalization constant. Next, we recall that the inverse of the function f given by f (LW) = LW exp{LW} is Lambert’s W-function denoted here by LW(f ) [627]. Then, we introduce the distortion function G(z) = z exp{κz/Q} and its inverse function G−1 (z) given by G−1 (z) = Q LW(κz/Q)/κ. Thus, we get Q κ Pst (q) = LW W (q) , (7.234) κ Z Q where Z is determined by the requirement Pst (q) dq = 1. In sum, (7.229) and (7.234) define the stationary Haissinski solutions of the Vlasov–Fokker– Planck equation (7.227). Note that an expression similar to (7.234) can also be derived using alternative reasoning [577].

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For κ = 0 we have LW (z) = z, Z = 1 and Pst (q) = W (q). That is, we deal with a Gaussian distribution. For κ > 0 we can read off from (7.228) that particles are driven away from regions of high density (because P (q, t) acts as a potential) and, consequently, the distributions Pst (q) are wider than the Gaussian distribution W (q). For κ < 0 particles are attracted by regions of high density (because now −P (q, t) acts as a potential) and, consequently, we deal with squeezed distributions and the distributions Pst (q) are smaller than the Gaussian distribution W (q), see Fig. 7.9. Since the parameter κ reflects the impact of the wakefield and the interactions between beam particles, we see that the particle-particle interactions can result in general in a distortion of the Gaussian distribution W (q) and in particular in a squeezing or widening of the beam particle distribution Pst (q).

κ0

0.1

–4 –3 –2

–1

0

1

2

3

q

4

Fig. 7.9. Haissinski distributions given by (7.234) for Q = 5 and several parameters of κ: broadened distribution for κ = 15 (solid line), Gaussian distribution for κ = 0 (dashed line), and squeezed distribution for κ = −10 (solid line); reprinted from c 2003, with permission from Elsevier [177],

Now let us simulate the Langevin equation (7.228). To this end, we interpret (7.228) as a self-consistent Langevin equation and solve it by means of the averaging method. That is, we discretize (7.228) by means of the Euler forward scheme l qn+1 = qnl + ∆t pln ,

pln+1 = pln 6 −∆t

qnl

7 2 L κ 1 qnl − qnk l k √ [qn − qn ] exp − + γpn − 2 ∆x (L − 1) 2π[∆x]2 k=1

√ + D∆t wnl ,

(7.235)

where qnl and pln are realizations of the random variables q(tn ) and p(tn ) at time points tn = n∆t. For details, see Sect. 3.4.4. Figure 7.10 (left panel)

348


P(p) 0.18

P(q) 0.16

0.1

0.1

–6

–4

–2

0

2

p4

6

–6

–4

–2

0

2

q4

6

Fig. 7.10. Left panel: Gaussian stationary distribution Pst (p) of the Vlasov–Fokker– Planck equation (7.227) as obtained from the analytical expression (7.229) (solid line) and the simulation of the Langevin equation (7.228) by means of (7.235) (diamonds). Right panel: Haissinski distribution Pst (q) computed from (7.234) (solid line) and the Langevin equation (7.228) (diamonds). Parameters: Q = 5, κ = 15, γ = 1 (L = 25000, ∆t = 0.03, 2[∆x]2 = 0.1, pl0 = q0l = 0, evaluation of the c 2003, stationary case pn , qn at n = 200, wn via Box–Muller); reprinted from [177], with permission from Elsevier

P(p) 0.18

0.2

P(q)

0.15 0.1

0.1 0.05

–6

–4

–2

2

p4

6

–6

–4

–2

2

q4

6

Fig. 7.11. Left panel: Gaussian distribution Pst (p) for κ = −10 computed from (7.229) (solid line) and the Langevin equation (7.228) (diamonds). Right panel: Haissinski distribution Pst (q) for κ = −10 computed from (7.234) (solid line) and the Langevin equation (7.228) (diamonds) (parameters other than κ as in Fig. 7.10); c 2003, with permission from Elsevier reprinted from [177],

shows Pst (p) computed from the random walk model (7.235) for κ > 0 and shows for the sake of comparison the exact result given by the Gaussian distribution (7.229). Figure 7.10 (right panel) shows the Haissinski distribution Pst (q) as obtained from the simulation of (7.235) for the same parameter value κ and as computed from (7.234). Figure 7.11 (right panel) shows the Haissinski distribution Pst (q) in the case of κ < 0 as obtained from the simulation of the Langevin equation (7.228) by means of (7.235) and as computed

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from (7.234). We have also computed the distribution Pst (p) for this parameter value. The result is shown in Fig. 7.11 (left panel) and is equivalent to the distribution Pst (p) shown in Fig. 7.10 (left panel) – as predicted by the theory. Figures 7.10 and 7.11 illustrate that we can describe the single particle dynamics of a particle ensemble satisfying the Vlasov–Fokker–Planck equations (7.227) by means of the corresponding Langevin equation (7.228) and its discretization (7.235). Haissinski Distributions – General Case Our considerations can easily be generalized to systems with wakefields HW = κM0−1 δ(q − q ) and single particle Hamiltonians H0 = p2 /2 + V (q), where V (q) describes a potential with respect to the generalized coordinate q. Then, (7.227) is replaced by ∂ ∂ ∂P (p, q, t) ∂P (p, q, t) dV + κ P (q, t) − P (p, q, t) + p dq ∂q ∂t ∂q ∂p ∂ ∂2 =γ (7.236) [pP (p, q, t)] + D 2 P (p, q, t) . ∂p ∂p Likewise, we need to replace (7.228) by d q(t) = p , dt √ d ∂ p(t) = − [V (q) + κP (q, t)] − γp + D Γ (t) . dt ∂q

(7.237)

Stationary solutions are given by Pst (p, q) = Pst (p)Pst (q) with Pst (p) defined by (7.229) and Pst (q) given by (7.234), where W (q) now corresponds to the Boltzmann distribution W (q) =

exp {−V (q)/Q} , exp {−V (q)/Q} dq

(7.238)

with Q = D/γ. 7.4.3 Noise Generator As pointed out by Primak and colleagues, Langevin equations involving probability-dependent diffusion terms can be used to model noise sources [488, 489]. We will briefly dwell on this issue and discuss this idea from the perspective of nonlinear Fokker–Planck equations. In particular, we will show that Primak’s noise generators can be described in terms of probability density maintaining nonlinear Fokker–Planck equations [165]. Our departure point is the trivial nonlinear Fokker–Planck equation

350


∂ P (x, t; u) = 0 , ∂t

(7.239)

for a random variable X(t) ∈ Ω = lR. Equation (7.239) states that P (x, t; u) is equivalent to the initial distribution u(x) for all t ≥ t0 . We assume now that there exists a constant C such that u(x) satisfies the relation ⎡ ⎤

x 1 ⎣ C − y u(y) dy ⎦ < ∞ . ∀x : 0 < (7.240) u(x) −∞

For example, for symmetric probability densities (u(x) = u(−x)) we can choose C = 0. Next, we interpret the right-hand side of (7.239) according to ∂ ∂ ∂ P (x, t; u) = k1 xP (x, t; u) − k1 xP (x, t; u) ∂t ∂x ∂x ⎡ ⎤

x ∂2 ∂ 1 ⎣C − y P (y, t; u) dy ⎦P (x, t; u) , xP (x, t; u) + k1 = k1 ∂x ∂x2 P (x, t; u) −∞ D2 (x, P ) (7.241) with k1 > 0. Note that on account of the inequality (7.240) and the observation P (x, t; u) = u(x) the diffusion coefficient D2 (x, P ) is well-defined and positive. By means of (7.241) we can now define a Markov diffusion process that satisfies (7.239). To this end, we consider initial distributions P (x, t, u) = Pst (x) = u(x) for which the conditional probability densities ∂ ∂ ∂2 D (x, u)P (x, t|x , t ; u) , P (x, t|x , t ; u) = k1 xP (x, t|x , t ; u) + ∂t ∂x ∂x2 2 (7.242) with ⎡ ⎤

x 1 ⎣C − D2 (x, u) = D2 (x, P ) = k1 y u(y) dy ⎦ (7.243) u(x) −∞

correspond to Markov transition probability density. In this case, (7.239) is a strongly nonlinear Fokker–Planck equation and, consequently, the Ito– Langevin equation that corresponds to (7.239) (or, more precisely, to the interpretation of (7.239) in terms of (7.242)) is given by # ⎡ ⎤ $

x $ d $ k1 ⎣ X(t) = −k1 X(t) + % C − y Pst (y) dx⎦ Γ (t) . (7.244) dt P (x; u) −∞ x=X(t)

The probability density Pst (x) occurring in (7.244) may be computed from Pst (x) = u(x) (two-layered Langevin equation) or from Pst (x) = δ(x − X(t))

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351

(self-consistent Langevin equation). For details, see Chap. 3. Equation (7.244) provides us with a convenient tool to generate a stationary stochastic process with a particular distribution Pst (x) = u(x) and a particular time scale k1 . That is, we can supplement a stochastic process that is given by a distribution Pst (x) with a process time scale k1 . Since both properties (Pst and k1 ) can be chosen independently, it has been suggested to use the Ito–Langevin equation (7.244) as a noise generator in engineering problems [488]. 7.4.4 Accuracy-Flexibility Trade-Off At first sight, one may think that for biological systems flexibility and accuracy are an antagonistic pair. The more accurately tasks are carried out, the slower the performance. That is, it seems to be plausible that flexibility can only be increased at the cost of accuracy. In fact, there is a reciprocal relationship between performance time and performance accuracy of humans, which is known as Fitts’ law [160, 433, 445, 499]. Fitts’ law states that the faster movements are performed, the less accurate they are. Therefore, it is safe to say that biological systems have to deal with a trade-off between accuracy and flexibility. Having said that we realize, however, that biological systems can usually handle that problem. Many biological systems possess the ability to adapt quickly and adequately to environmental and internal changes and in this sense show both accuracy and flexibility. For example, humans and animals match their gaits to locomotory speeds in order to minimize energy consumption. Consequently, they switch from one gait to another at particular velocities [12, 299, 426, 427]. Similarly, when performance speed is increased, humans tend to abandon movement patterns requiring a high degree of coordination and show involuntary switches to simpler and more stable coordination patterns. For example, this has been observed for rhythmic isofrequency finger and wrist movements [109, 110, 216, 336, 339, 461], paced unimanual arm movements [471], and polyrhythmic tapping [50, 133, 475] (see also Sect. 5.5.6). Furthermore, perceptual patterns of apparent motion change qualitatively when the frequency of stroboscopically presented objects is increased [195, 266, 357, 521]. In the regions preceding and following transition regions, the performed patterns usually exhibit a high degree of accuracy [339, 475]. Similarly, in the preand posttransition regions of perceived apparent motions, humans describe their visual experiences in terms of meaningful perceptual patterns. In sum, we have given examples of qualitative changes in locomotion, coordinated movements, and perception under critical task conditions. In these examples, transitions between well-defined (and in this sense accurate) spatio-temporal motoric and perceptual patterns are observed and the perception-action systems of interest are characterized by both flexibility and accuracy. Therefore, at issue is to clarify how flexibility and accuracy can be implemented in a system at the same time. In this context, it has been shown that stochastic processes that involve a particular kind of stochastic feedback,

352


namely, negative stochastic feedback, exhibit a relatively small accuracyflexibility trade-off [190, 196]. Negative Stochastic Feedback Model Our departure point is the Langevin equation d X(t) = h(X) + Q g (P (x, t; u))|x=X(t) Γ (t) , dt

(7.245)

for t ≥ t0 and X ∈ Ω = lR with X(t) distributed according to u(x) at t = t0 . We assume that this Langevin equation is related to a strongly nonlinear Fokker–Planck equation. Then, in line with Sect. 3.4, the probability density P is either computed in a self-consistent fashion from X(t) or is taken as the solution of this nonlinear Fokker–Planck equation. Interpreting (7.245) as an Ito–Langevin equation, as shown in Sect. 3.4, the corresponding strongly nonlinear Fokker–Planck equation reads ∂ ∂ ∂2 P (x, t; u) = − hP + Q 2 g 2 (P )P . ∂x ∂x ∂t

(7.246)

If we put g (x, t) = g(P (x, t; u)) and interpret (7.245) as the Stratonovich– Langevin equation d X(t) = h(X) + Q g (X, t)Γ (t) , dt Stratonovich

(7.247)

then from the equivalence −

Q ∂[g ]2 + Q g (X, t)Γ (t) = Q g (X, t)Γ (t) 2 ∂X Ito Stratonovich

(7.248)

(see e.g. [298, Sect. 5.4.2]) it follows that (7.247) is related to the nonlinear Fokker–Planck equation ∂ ∂g(P ) ∂2 ∂ P (x, t; u) = − h(x) + Q g(P ) P + Q 2 g 2 (P )P . (7.249) ∂t ∂x ∂x ∂x We will deal with both cases simultaneously by studying the evolution equation ∂g(P ) ∂ ∂ ∂ P (x, t; u) = − h(x) + 2Q(1 − ) g(P ) P − Q g 2 (P )P . ∂x ∂x ∂x ∂t (7.250) That is, P (x, t; u) of (7.250) is equivalent to P (x, t; u) = δ(x − X(t)) derived from the Langevin equation (7.245) if we interpret (7.245) according to Ito

7.4 Applications

353

calculus and put = 1 or if we interpret (7.245) according to Stratonovich calculus and put = 1/2. Furthermore, we assume that h is the force of x a globally attractive potential. That is, we have V (x) = − h(x ) dx and V (x → ±∞) → ∞. Finally, we require that g(z) satisfy the conditions g≥0,

∂g ≤0, ∂z

(7.251)

for z ≥ 0. Qualitative Discussion: Stationary Case Let us discuss qualitatively the impact of the function g on the stationary behavior of a statistical ensemble described by (7.250) and (7.251). For g = 1, the Fokker–Planck equation is linear with respect to P and the stationary probability density is given by the Boltzmann distribution 1 V (x) , (7.252) W (x) = exp − ZB Q with ZB = Ω exp{−V (x)/Q}dx. The positions of the maxima of the stationary probability density (7.252) correspond to the positions of the minima of the potential V . For ∂g/∂P < 0, however, the maxima of the probability √ density P describe minima of the noise amplitude Qg(P ). Consequently, in the stationary case, members of a statistical ensemble that are located in close vicinity of the minima of V are less affected by noise than members at other positions. By comparison with the trivial case g = const, this mechanism results in a more pronounced aggregation of ensemble members at the minima of the potential V . We can also look at this effect in a different way. We may say that the nonlinearity g(P ) “distorts” the probability density W such that large values are enhanced whereas small values are weakened. Roughly speaking, we anticipate that due to the inequality ∂g/∂P < 0 we have the following circular causality: the more probable a stable state related to a potential minimum is, the less it will be affected by noise and, conversely, the less the stable state is affected by noise, the more probable it is. Therefore, we may say that (7.245-7.251) describe processes with negative stochastic feedback [190, 196]. Next, let us examine in a more quantitative manner stationary solutions of the negative stochastic feedback model. Stationary Solutions Equation (7.250) corresponds to the nonlinear Fokker–Planck equation (2.10) with D1 (x, P ) = h + 2Q(1 − ) g(P )∂g(P )/∂x and D2 (P ) = Qg 2 . Consequently, stationary distributions of (7.250) satisfy (2.23). Since we are looking for solutions with P (x → ±∞) = 0 (natural boundary conditions), the probability current J vanishes and we obtain

354


∂ g 2 (Pst ) ∂Pst h(x) = g 2 (Pst ) + . Pst ∂x Q ∂x By virtue of (7.252) and (7.253), the implicit equation

Pst 2 1 g (z) W (x) = exp g 2 (Pst ) + dz = f (Pst ) Z z

(7.253)

(7.254)

can be found. The variable Z guarantees the normalization of Pst . The function f describes the mapping of the probability density Pst (x) to W (x) and can be regarded as a distortion function similar to the distortion functionals discussed in Sects. 4.7.1 and 7.2.4. Assuming that f is invertible with F = f −1 , we can compute Pst from W by means of 1 Pst (x) = F W (x) . (7.255) Z In order to illustrate this procedure, we put g(P ) = gn,α with gn,α =

1 1 + αP

n/2 , α ≥ 0, n = 1, 2, 3, . . .

(7.256)

Note that for α = 0 we have gn,α = 1 and the nonlinear Fokker–Planck equation becomes linear. Substituting (7.256) into (7.254), we obtain [144] fn,,α (Pst ) = n−1 n − 1 (−αPst )k Pst exp + + Cn 1 + αPst (1 + αPst )n k(1 + αPst )k k

.

k=1

(7.257) The constants Cn can assume arbitrary values and can be compensated by the normalization Z. Focusing on weak nonlinearities (n = 1, 2), we choose C1 = 0, C2 = 1 and obtain Pst f1,,α (Pst ) = , exp 1 + αPst 1 + αPst Pst 1 f2,,α (Pst ) = . (7.258) exp + 1 + αPst (1 + αPst )2 1 + αPst Properties of the Distortion Functions Figure 7.12 shows the distortion functions fn=(1,2),,α for both the Ito and the Stratonovich case. In the limit Pst → ∞ the distortion functions fn=(1,2),,α (Pst ) converge to a finite value 1/α. Consequently, all the functions F1,=1/2,α , F1,=1,α , and F2,=1/2,α have a singularity at 1/α. This

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355

implies that in order to map W onto Pst (see (7.255)) the normalization constant Z must satisfy the inequality 1/α < max{W (x)}/Z. Figure 7.12 demonstrates that the functions F describe mappings W → Pst such that large values of W are amplified and small values of W are weakened. Finally, note that a detailed analysis reveals that f2,=1/2,α (z) (Stratonovich case) as a function of z is a strictly concave function, whereas f2,=1,α (z) (Ito case) has a maximum at Pst = 1/α with a value 1/(2α) exp{3/4} > 1/α. For this reason, we only consider the lower branch of F2,1,α , that is, the lower branch of the curve in the inlet of Fig. 7.12 corresponding to graph IV . αf IV 1.00

III II

0.75

I

F

0.50 0.25

1.0

2.0

3.0

4.0

αPst

Fig. 7.12. Distortion function fn,,α as a function of Pst for n = 1 (I, II) and n = 2 (III, IV ): the Ito case ( = 1 : II, IV ) results in stronger distortions than the Stratonovich calculus ( = 1/2 : I, III); the inlet shows the inverse graphs c 2002 Kluwer Academic Publishers, Fn,,α = f −1 n, , α; reprinted from [196], with kind permission of Kluwer Academic Publishers

Double-Well Potential In order to analyze further properties of the mapping W → Pst , we choose a particular deterministic force h. We consider h(x) = −dV /dx with V (x) = −

k1 2 k2 3 k3 4 x + x + x 2 3 4

(7.259)

and k1 > 0, k2 > 0, and k3 > 0, which has a maximum at the origin and both a local and a global minimum, see Fig. 7.13. The Boltzmann distribution W of this potential can be computed by means of (7.252). To obtain a normalized solution of (7.255), we generate a family of distribution functions Pi (x; Zi ) that are regarded as candidates for Pst by applying Fn,,α to W for various Zi . Explicitly, we initially estimate Z0 , integrate over P0 (x; Z0 ), and use the resulting value to estimate a new approximation of Z1 , which gives us P1 (x; Z1 ). This procedure is repeated iteratively until convergence. Final estimates of the probability densities are given in Fig. 7.13. The undeformed probability density (gn,α = 1, curve (i)) shows a much lower probability at the

356


global minimum of the potential compared to the cases including nonlinear feedback (see curves (ii) and (iii)). P0 V

1.5

(iii) 1.0

(ii) 0.5

(i)

-2.5

0.0

2.5

x

Fig. 7.13. Stationary probability density Pst (x) of (7.250) with g and h given by (7.256) and (7.259), respectively. Parameter values are (i) g = 1, (ii) n = 1, = 1, and (iii) n = 2, = 1/2 ; α = 1, Q = 50, k1 = 50, k2 = k3 = 100. The inlet shows c 2002 Kluwer Academic the corresponding potential V (x); reprinted from [196], Publishers, with kind permission of Kluwer Academic Publishers

Transient Solutions Let us discuss now the transient behavior of solutions of the Langevin equation (7.245). To this end, we consider the Ito case for a weak nonlinearity and choose n = 1 in (7.256). Then, (7.245) reads Q ∂ X(t) = h(X) + Γ (t) . (7.260) ∂t 1 + αP (x, t) x=X(t)

Likewise, (7.250) reads ∂ ∂ ∂2 P P (x, t; u) = − h(x)P + Q 2 ∂t ∂x ∂x 1 + αP

(7.261)

and is equivalent to (7.70) discussed in Sect. 7.2.2. In Sect. 7.2.2 we have shown that (7.261) is an entropy Fokker–Planck equation of the form (6.1) involving the entropy measure NSFSα defined by (7.72). Since NSFSα is a strictly concave measure (see Sect. 6.4.2), the free energy F = V − Q NSFSα is bounded from below (case A in Table 4.2) and the H-theorem for free energy Fokker–Planck equations applies. Thus, we conclude that transient solutions of (7.261) converge to stationary ones in the long time limit. The Langevin equation (7.260) was solved numerically using the histogram method for self-consistent Langevin equations, see Sect. 3.4.4. Figures 7.14 and 7.15 show the solutions for two different parameter values of

7.4 Applications

0.01

357

H(x)

0

-10 -5 0

x

5 10

t7

t6

t5

t4

t3

t2

t1

t0

Fig. 7.14. Simulation of the Langevin equation (7.260) with g and h given by (7.256) and (7.259), respectively. Numerical results are plotted at different times ti with ti+1 > ti . The dashed line in front corresponds to the analytical result, see Fig. 7.13 (ii). The histogram method for self-consistent Langevin equations was used. Parameters: α = 1, Q = 50, k1 = 50, k2 = k3 = 100 (L = 40000, ∆t = 1/1000, c 2002 Kluwer Academic ∆x = 1/100, wn via Box–Muller); reprinted from [196], Publishers, with kind permission of Kluwer Academic Publishers

H(x) 0.4

0.2

0 -10 -5 0

x

5

t7

t6

t5

t4

t3

t2

t1

t0

Fig. 7.15. Simulation results for α = 100 (other parameters as in Fig. 7.14); c 2002 Kluwer Academic Publishers, with kind permission of reprinted from [196], Kluwer Academic Publishers

α. In the stationary case, the maximum pm of P is located at the global minimum xm of the potential (7.259). The numerical simulation for a weak nonlinearity is in good agreement with the analytical solution given above, see Fig. 7.14. If we increase the nonlinearity, the maximum value of the probability density pm = P (xm ) increases and the variance K decreases, which results in sharply peaked distributions as shown in Fig. 7.15. In this case, the transient probability densities are essentially described by two peaks that correspond to the two minima of the potential. Therefore, the stochastic process primarily consists of discrete jumps between the minima of the potential. The probability to find realizations of the stochastic process outside close vicinities of the potential minima becomes negligible.

358

7 General Nonlinear Fokker–Planck Equations pm 12.5 10.0 7.5

C

5.0

B

2.5

A 1.0

2.0

3.0

4.0

5.0

6.0

t

Fig. 7.16. Maximal probability pm as function of time t. Stochastic processes with negative stochastic feedback (α = 5: curve B and α = 20: curve C; Q = 50) show shorter transient parts compared to the reference process without stochastic c 2002 Kluwer Academic feedback (α = 0, Q = 4.5: curve A); reprinted from [196], Publishers, with kind permission of Kluwer Academic Publishers K 1.00 0.75

A 0.50

C B

0.25

1.0

2.0

3.0

4.0

5.0

6.0

t

Fig. 7.17. Variance K as a function of t (parameters as in Fig. 7.16); reprinted c 2002 Kluwer Academic Publishers, with kind permission of Kluwer from [196], Academic Publishers

In order to compare transition times for systems with and without stochastic feedback, we adjusted the parameters α and Q in such a way that the stationary probability densities have approximately either the same peak probability density pm or the same variance K. Figures 7.16 and 7.17 show the results of these simulations. The graphs A, B, and C were computed from three different processes, which will be referred to as A−, B−, and C−processes, respectively. The A−process corresponds to the conventional stochastic process given by (7.245) with g = 1. The B− and C−processes correspond to processes with stochastic feedback. The parameters α and Q are chosen such that the stationary peak probabilities pm of the A− and B−processes and the stationary variances K of the A− and C−processes assume the same values. In comparison to the relaxation processes defined by the ordinary Langevin equation (curves A in Figs. 7.16 and 7.17), the impact of the negative stochastic feedback results in a much faster relaxation to stationary values of pm (see Fig. 7.16). Stronger nonlinearities again

7.4 Applications

359

increase the probability pm at xm (curve C in Fig. 7.16). The stationary variance decreases with increasing α (compare tails of curves B and C of Fig. 7.17), because increasing α implies that the effective diffusion coefficient Q/(1 + αP (x)) decreases for states x with P (x) > 0. From Fig. 7.17 it is clear that the variances of systems with stochastic feedback converge to their stationary values much faster than the variances of systems without stochastic feedback. Towards a Minimization of the Accuracy-Flexibility Trade-Off We have illustrated that the aggregation of the subsystems of a many-body system in the minimum of a potential (related to some kind of energy or effort) can be amplified by means of negative stochastic feedback and that the transition times are significantly shorter than those of comparable systems without feedback. Consequently, a biological system under the impact of negative stochastic feedback can detect the position of the minimum value of a potential force with a large probability and within a short transient period. In other words, such a system exhibits the ability to generate sharply peaked probability densities and to respond quickly to changes in both the environment and its internal parameters. Moreover, the form of (7.245) does not require any a priori knowledge about the underlying potential force. Thus, the system can be considered to be self-organized. Bose Systems and Negative Stochastic Feedback In closing this section, we would like to point out that Bose systems can be considered as another example of systems with negative stochastic feedback. To this end, let us consider for = 1 the nonlinearity 0 ln[1 + P ] gBE (P ) = , (7.262) P which leads to the Fokker–Planck equation ∂ ∂ ∂ P (x, t; u) = − h(x)P + Q ln[1 + P ] . ∂t ∂x ∂x

(7.263)

This evolution equation, in turn, corresponds to the Fermi Fokker–Planck equation (6.306) if we put M0 = 1 and Q = T . The stationary probability density of (7.263) reads Pst (x) =

1 exp{(U0 (x) − µ)/Q} − 1

,

(7.264)

and describes a Bose–Einstein statistics. Just as in our first example (see (7.256)), in the limit P → 0 the nonlinearity gBE converges to unity (which

360


can be shown by applying the rule of de l’Hopital to [gBE ]2 ). Moreover, for low density distributions, the diffusion term of (7.263) is approximately given by ln[1 + P ] ≈ P / [1 + 0.5P ]−1 + O(P 3 ). That is, up to terms of the order of two, the nonlinear Fokker–Planck equation for Bose particles (7.263) is equivalent to (7.261) with α = 1/2. Furthermore, we obtain P 1 d gBE (P ) = Z(1 + P ) , (7.265) dP 2P 2 (1 + P ) ln[1 + P ] where Z(y) is defined by Z(y) = y −1−y ln y for y > 1 (P > 0) and Z(1) = 0. Since the inequality ln z < z − 1 holds for z > 0 and z = 1, it follows that Z(y) < 0 for y > 1 (hint: substitute z by 1/y). Consequently, gBE satisfies (7.251) and Bose systems can be regarded within the Fokker–Planck approach as systems with negative stochastic feedback.

7.5 Bibliographic Notes In this section, we will address some studies that are concerned with free energy Fokker–Planck equations, entropy Fokker–Planck equations, and nonlinear Fokker–Planck equations in general and have not been mentioned so far. In doing so, we will not give a review on the subject of nonlinear Fokker– Planck equations but we will illustrate the variety of topics that have been discussed in the context of nonlinear Fokker–Planck equations. Natural Boundary Conditions K-Model with Additive Noise Pioneering works on the K-model discussed in Sect. 5.1.5 have been carried out by Desai and Zwanzig [135] and Kometani and Shimizu [352]. The free energy approach to the K-model is due to Shiino [522, 523]. The K-model and various modifications concerning the drift coefficient of the model have been discussed in the literature [30, 32, 77, 88, 127, 128, 141, 142, 295, 393, 431, 435]. K-Model with Multiplicative Noise The K-model with multiplicative noise has also been studied [20, 59, 392, 434, 644, 645]. In this context, discontinuous phase transitions [434], discontinuous phase transitions related to reentrant bifurcations [644], the impact of colored noise on reentrant bifurcations [392], and propagation of signals in cellular media [645] have been examined.

7.5 Bibliographic Notes

361

K-Model and Spatially Extended Systems The K-model with multiplicative noise has been used as a mean field approximation of spatially distributed systems with diffusive coupling (i.e., coupling described by the Laplacian operator or next neighbor coupling) [219, 220, 224, 288, 601, 600, 602]. Pattern Formation The formation of spatial patterns in spatially distributed systems with diffusive coupling and multiplicative noise sources has been studied by means of nonlinear Fokker–Planck equations [220, 466, 646]. Multiple Species and Relaxation Oscillators Multivariate nonlinear Fokker–Planck equations involving nonlinear drift terms like in the K-model have been studied in several studies. In these studies the components of the respective random vectors correspond to different kinds of subsystems or species [123, 218, 649]. For example, Yamaguchi and co-workers have studied the collective behavior of coupled relaxation oscillators [638, 639]. Schuster and Wagner have considered a Wilson– Cowan model that comes with two dynamical variables for each oscillatory subunit [513, 514]. In order to study mean field coupled networks of oscillatory neurons, single neurons have been modeled by means of the twodimensional Morris–Lecar system [272] and the FitzHugh–Nagumo equation [280, 320, 462]. Kawai and colleagues have studied a two-component mean field model that describes self-sustained oscillations in terms of a timedependent probability density and a nonstationary oscillating order parameter [330]. Inertia Effects Multivariate nonlinear Fokker–Planck equations and related models taking inertia effects into account have also been considered. In these studies the focus was on the formation and breakup of swarms [420, 516], reentrant bifurcations [330], and the impact of parametric driving forces [54]. In addition, changes of the crystallographic structure of matter (so-called structural phase transitions) have been addressed in the context of the independent-site approximation, which is some kind of mean field approximation [80, 161]. Surface Physics Solutions of the Kadar–Parisi–Zhang equation have been examined by means of nonlinear Fokker–Planck equations [225, 404]. In doing so, the growth of surfaces and roughening phenomena have been studied. In addition wetting processes [132] have been described by nonlinear Fokker–Planck equations.

362


Particle Sedimentation Particle sedimentation in fluids has been modeled by means of a multivariate Langevin equation with probability-dependent coefficients [290]. Roughly speaking, the model is given by the Langevin equation d X(t) = V (t) , dt d V (t) = −γX + a(X) + b(K(X))Γ (t) , dt where a(z) and b(z) are functions of z.

(7.266) (7.267)

Batchelor and Turbulent Diffusion As early as 1952, Batchelor proposed the diffusion equation ∂ ∂2 (7.268) P (x, t; u) = Q 2 X 2 P (x, t; u) ∂t ∂x in order to describe the displacement of particles in turbulent fields [40]. Equation (7.268) has a structure similar to the model discussed in Sect. 7.3.3. Stochastics of Ion Channels Ion channels of neurons can be regarded as two-state systems. Accordingly, at an ion channel one may find an ion either inside or outside the membrane of a neuron. Let X1 ≥ 0 and X2 ≥ 0 denote the occupation numbers of these states. In line with the quantum mechanical description of lasers [256], it has been suggested that X = (X1 , X2 ) satisfies the Langevin equation d −w21 w12 X(t) = X + G(X1 , X2 ) · Γ(t) , (7.269) w21 −w12 dt where G describes a 2 × 2 matrix that depends on the mean values X1 and X2 [262]. It is clear from (7.269) that the corresponding Fokker–Planck equation involves a diffusion coefficient that depends on X1 and X2 as well. That is, the system is described by means of a nonlinear Fokker–Planck equation. Periodic Boundary Conditions Winfree and the Theory of Synchronization Much of our interest in the behavioral synchronization of populations was fueled by Winfree’s seminal works on that topic [632, 633]. The original model proposed by Winfree differs slightly from the KSS model studied in this chapter and in Sect. 5.3.2. While the KSS model involves a mean field coupling term k UMF (Xi −Xk ), the Winfree model exhibits a coupling term given by A(X k ). Models of this kind have also been considered in the more recent k literature [27, 391].


363

KSS Model with Distributed Eigenfrequencies The KSS model discussed in Sect. 7.3.1 describes an ensemble of phase oscillators with a common eigenfrequency ω. Taking a more general point of view, we may think of ensembles of coupled oscillators with different eigenfrequencies. In this context, the question arises as to what extent oscillators with different eigenfrequencies synchronize their behavior. For systems that are not subjected to fluctuating forces, this question and related issues have been studied in [115, 363, 365, 367, 368, 369, 443, 504, 505, 513, 514, 554, 553, 564, 565, 563, 603, 620, 640, 647] for timecontinuous systems and in [112, 113, 114, 575] for time-discrete systems. Oscillator populations with some kind of distributed state-dependent eigenfrequencies have been considered in [599]. Taking fluctuating forces into account and using nonlinear Fokker–Planck equations, the behavior of oscillator populations with distributed eigenfrequencies has been studied in [4, 26, 60, 61, 63, 62, 96, 102, 103, 364, 365, 366, 477, 503, 542, 555, 643]. For reviews, see [552, 557]. Such coupled oscillator models have been used to describe associative memories [369, 640, 643]. A coupled oscillator population that is subjected to white noise fluctuating forces, on the one hand, and exhibits eigenfrequencies that fluctuate according to a dichotomic Markov process, on the other hand, has been studied as well [355]. Multiplicative Noise The KSS model with sine-coupling and the mean field HKB model for systems with multiplicative noise have been studied in [343, 341, 344, 463, 491, 492]. Delays Mean field models including delays have also been investigated in the context of nonlinear Fokker–Planck equations [342, 450, 642]. In particular, the phenomenon of stochastic resonance has been addressed [342]. Higher Order Coupling Functions Models similar to the KSS model that involve higher order coupling functions such as sin(2x), sin(3x), . . . instead of the sine-coupling function have been studied in [25, 117, 118, 119, 275, 365]. Inertia Effects The dynamics of mean field coupled phase oscillators under the impact of inertia effects and related models have attracted considerable attention [5, 22, 23, 24, 159, 226, 380, 381, 382, 383, 384, 385, 477, 562, 581]. For example, Daido has studied the circadian rhythms using arrays of two-component oscillators [120]. Coupled phase oscillators that take some kind of inertia effects into account have been examine by Hadley et al. in the context of phase

364


locking in arrays of Josephson-junctions [248]. In a similar vein, Acebron et al. have focused on the synchronization of coupled phase oscillators with inertia terms [6]. Parkinson’s Disease Several authors have suggested that Parkinsonian tremor is caused by populations of neurons that synchronize their oscillatory activity [390]. In a series of papers, Tass [569, 570, 571, 572, 573, 574] proposed a model of coupled neural oscillators that are putatively involved in Parkinsonian tremor (see also [568]). According to this oscillator model, the couplings between neural oscillators in healthy people are so weak that they do not lead to the degree of synchronization necessary to create Parkinsonian tremor. The oscillators are said to be de-synchronized. In contrast, in patients with Parkinson’s disease, the oscillators are assumed to be strongly connected with each other. Due to these connections, a mean field force emerges and results in a self-organized synchronization of the oscillator population. This synchronization, however, can be destroyed by stimulating the synchronized neurons with an appropriate external signal. In other words, it is believed that an external signal can be used to de-couple neural oscillators. The hope is that this de-coupling mechanism can be applied to help patients suffering from Parkinson’s disease. Miscellaneous Topics In addition to the aforementioned applications, mean field models for periodic random variables have been used to describe Josephson arrays [629, 630], Landau damping [556], arrays of semi-conductor lasers [356], charge density waves [60], and have been proven to be useful tools for the study of coupled neurons described by Hodgkin–Huxley equations [272, 276]. Nonlinear Diffusion Equations Nonlinear diffusion equations and their applications are discussed in Crank’s book [101], whereas mathematical aspects of nonlinear diffusion equations are addressed in the Proceedings by Ni et al. [446]. As illustrated in Chap. 6, such nonlinear diffusion equations are closely related to entropy Fokker–Planck equations involving entropy measures different from the Boltzmann entropy. A discussion on the renormalization group approach to the Barenblatt–Pattle solutions of the porous medium equation can be found in [229]. Mathematical Literature In the mathematical literature, nonlinear Fokker–Planck equations have been investigated in line with a seminal study by McKean Jr. [411] (see Sect. 3.1) and are sometimes referred to as McKean–Vlasov equations [73, 217, 222, 414,


365

454]. In this context, the propagation of molecular chaos (see Sect. 3.8) has been addressed [414, 415]. Stochastic processes related to nonlinear FokkerPlanck equations have also been called processes depending on Brownian paths [452]. The convergence of transient solutions of nonlinear Fokker– Planck equations to stationary ones has been examined by means of functionals that are similar to the Lyapunov functionals discussed in Chap. 4 and in this chapter, see, for example, [30, 31, 32, 87]. The relationship between Langevin equations similar to the ones presented in Sect. 3.4 and nonlinear Fokker–Planck equations has been studied in the context of so-called semilinear parabolic partial differential equations by Milstein and colleagues [423, 424, 425]. In a similar vein, it might be helpful to study nonlinear Fokker–Planck equations in the context of the theory of nonlinear parabolic partial differential equations [205, 206, 395].

8 Epilogue

One may raise the question: what is at the heart of this book? In reply, it may be said: it is the nonlinearity of nature. This book is concerned with nonlinear science in general and synergetic systems in particular. Nonlinear science tries to meet the demand of the modern society for analyzing and dealing with highly complex many-body systems. It is a rapidly growing field of science that lives in a triangle with corners at the theory, the numerics, and the experiment. In the preceding chapters we have shown that nonlinear Fokker– Planck equations are powerful tools to describe and understand various phenomena that are observed in the inanimate and animate world and arise due to the nonlinearity of systems. In recognition of the aforementioned triangle of nonlinear science, we have discussed nonlinear Fokker–Planck equations with an eye on theoretical physics, numerical solutions by means of Langevin equations, and top-down modeling of experimental findings. In this final chapter we would like to discuss two issues. The first issue concerns the top-down modeling by means of nonlinear Fokker–Planck equations and possible ways of its verification and falsification. The second issue is about generalizations. Both issues are somewhat of a speculative character. That is, we will not give final answers. Rather we will make some hypotheses. Top-Down Modeling and Its Verification and Falsification Although nonlinear Fokker–Planck equations can describe a variety of frequently observed phenomena, this does not imply that the underlying mechanisms are adequately described in terms of nonlinear Fokker–Planck equations. As usual, a particular phenomenon can be described by means of several models involving different notions about the fundamental mechanisms that give rise to the observed phenomenon. In this context, the problem is to select a particular model from a set of possible models that all do their job equally well. For example, if a system exhibits a power law distribution, we can describe the system by means of a nonlinear Fokker–Planck equation as shown in Chap. 6. Alternatively, one can describe power law distribution by means of linear Fokker–Planck equations with state-dependent diffusion coefficients. In the context of nonlinear Fokker–Planck equations, the establishment of states with power law distributions is regarded as a collective phenomenon. The notion is that a power law distribution arises from the

368

8 Epilogue

interactions between the subsystems of a many-body system. In the context of linear Fokker–Planck equations, power law distributions describe a single system that is subjected to a multiplicative noise source [65, 325, 436, 547] or to some kind of temperature fluctuations [42]. From this example we learn that we can make a choice of a particular model if there is additional information available that comes, for example, in terms of the microscopic structure of a system. Having said that, it would be beneficial if we could verify or falsify irrespective of such additional information a particular model just on the basis of the observed phenomenon, that is, on the basis of experimental data. In fact, there are data analysis techniques available that can be used to extract the model equations of systems described by Markov diffusion processes from experimental data [208, 209, 210, 494, 536]. In principle, such data analysis techniques could also be applied to extract the evolution equations of nonlinear families of Markov processes and, consequently, of systems described by strongly nonlinear Fokker–Planck equations. Accordingly, based on experimental observations one could determine whether the system under consideration is adequately described by means of a linear or nonlinear Fokker–Planck equation. In addition, one could determine the dependencies of the drift and diffusion terms on state variables and density measures. Let us illustrate the latter point. For example, let us consider a system that can be described by a univariate random variable X(t). Let us further assume that we have reason to believe that the system can be described by means of a strongly nonlinear Fokker–Planck equation with a diffusion coefficient D2 (x, P ) that does not explicitly depend on the state variable x but is a function (not a functional) of P , that is, we have D2 (x, P ) = D2 (P ). Then, we can compute D2 (x, t) = D2 (P (x, t)) by means of D2 (x, t) = D2 (P (x, t)) = lim

∆t→0

1 [X(t − ∆t) − X(t)]2 X(t)=x , 2∆t

(8.1)

see (3.81) and the references cited above. Likewise, we can compute the probability density P from B 2 C 1 1 x − X(t) , P (x, t) = δ(x − X(t)) = lim √ exp − ∆x→0 2 ∆x 2π∆x (8.2) see (3.49). If we regard now for a fixed time t and several x-values. the pairs (P (x, t), D2 (x, t)) as points of a two-dimensional plane and plot these points on the plane, then they will represent a graph that corresponds to the function P → D2 (P ). For example, for systems described by the nonlinear Fokker– Planck equation proposed by Plastino and Plastino that has been addressed in Chap. 6, this procedure will give us the graph D2 (P ) = P q−1 [200].

8 Epilogue

369

Generalizations As stated in Chap. 2, the nonlinear Fokker–Planck equation (2.4) does not describe the most general nonlinear Fokker–Planck equation that we can think of. We may think of generalizations concerning the drift and diffusion coefficients of (2.4), the transition probability densities related to solutions of (2.4), and the Fokker–Planck operator involved in (2.4). For example, a more general class of nonlinear Fokker–Planck equations may be given by nonlinear parabolic partial differential equations that have, roughly speaking, the same Fokker–Planck operator as the nonlinear Fokker–Planck equation (2.4) but have a more general type of drift and diffusion coefficients [205, 206, 395, 446]. Furthermore, in Chap. 3, we confined ourselves to discussing nonlinear Fokker–Planck equations in the context of linear evolution equations for transition probability densities. Alternatively, one may consider nonlinear Fokker–Planck equations related to nonlinear evolution equations for transition probability densities [67]. Finally, some of the concepts and methods discussed in this book may be applied to other types of evolution equations for probability distributions and density measures. In this context, we may think of Liouville equations, master equations, Boltzmann equations, fractional linear Fokker–Planck equations, and fractional nonlinear Fokker– Planck equations. For example, two concepts that have been frequently used in this book, namely, distortion functionals and Kullback measures related to concavity inequalities, have also found applications in the theory of nonlinear master equations, see (4.122) and [185]. Furthermore, the notion of Fokker-Planck equations determined by free energy measures may be applied to nonlinear reaction-diffusion equations as well [178].

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Index

Accuracy-flexibility trade-off, 351 Anomalous diffusion, 15 and nonextensivity, 219 Plastino–Plastino model, 251 porous medium equation, 250 Sharma–Mittal model, 274 Basins of attraction, 25 dynamical Takatsuji model, 140 multistable variability model, 339 BCS theory, 234 Bifurcation diagram bounded B(M1 )-model, 155 Desai-Zwanzig model, 152 dynamical Takatsuji model, 144 KSS model with sine coupling, 162 Maier–Saupe model, 200 multistable variability model, 339 reentrant phase transition, 331 Bistability, see Multistability Black body radiation model, 294 Boltzmann equation, 28 Boundary conditions, 23 Brownian particle, 1 Canonical-dissipative systems, 90 Chapman–Kolmogorov equation, 47 Chemical potential, 82 Classifications, 26 Cluster amplitude and cluster phase, 156 Continuity equation, 22 Continuous phase transitions, 187 Control parameters, 4 Correlation functions dynamical Takatsuji model, 144 Fluctuation–dissipation theorem, 70 Plastino–Plastino model, 258

Shimizu–Yamada model, 69 strongly nonlinear case, 36 Damping constant, 1 Damping force, 1 Darcy’s law, 248 Data analysis, 368 Discontinuous phase transitions, 187 Distortion functionals, 319 free energy case, 97 Lambert’s W-function, 346 negative stochastic feedback model, 354 Distributions Boltzmann distributions, 79 bunch-particle distributions, 342 cut-off distributions, 10 Plastino–Plastino model, 253 population dynamics, 297 porous medium equation, 250 Sharma–Mittal model, 264 Gaussians, 57 Haissinski distributions, 345 power law, 10 Plastino–Plastino model, 252 Sharma–Mittal model, 264 Drift and diffusion coefficients, 20 Drift and diffusion terms, 20 Drift- and diffusion forms, 222 Fermi and Bose systems, 280 Entropy and information measures, 224 derivation of entropies, 310 entropy increase, 218 entropy production, 81, 87 examples, 231 κ-entropy, 247 average information measure, 244

402

Index

Boltzmann entropy, 232 Fermi and Bose systems, 233, 289 Fisher information, 247 negative stochastic feedback entropy, 245 Renyi entropy, 236 Sharma–Mittal entropy, 239 Tsallis entropy, 238 vorticity entropy, 235 excess entropy, 304 properties, 224 concavity, 226 extensivity, 228 nonextensivity, 228 Families of Markov processes, 46 linear families, 47 nonlinear families, 48 Ferromagnetism, 140, 188 Finite difference schemes, 29 Fluctuating force, 1 Langevin force, 2, 37 Fluctuation–dissipation theorem, 70 Fourier and moment expansions, 29 Free energy K-model, 120 KA -model, 126 bounded B(A)-model, 126 bounded B(M1 )-model, 152 compensated B(A)-model, 122 Desai–Zwanzig model, 148 dynamical Takatsuji model, 140 entropy case, 213 Fermi and Bose systems energy phase space, 289 KSS model, 158 with sine coupling, 160 Maier–Saupe model, 197 mean field HKB model, 168 negative stochastic feedback model, 356 Shimizu–Yamada model, 136 Free energy principle, 75 GENERIC, 87 Gross–Pitaevskii equation, 3 Group behavior, 140, 206 H-Theorem

for stochastic processes, 43 free energy case, 77 linear nonequilibrium thermodynamics, 89 multistable variability model, 336 Hartree–Fock theory, 2 Heat bath, 1 Hitchhiker processes, 50 HKB potential, 167 Hysteresis, 200 Ito-Langevin equation, see Langevin equation Kinetical interaction principle, 28, 281, 323 Kramers equation, 92 Fermi and Bose systems, 285 linear nonequilibrium thermodynamics, 95 Tsallis entropy, 288 with generalized thermostatistics, 284 Kramers–Moyal coefficients, 34 Lagrange multiplier, 77 Landau theory, 4 Langevin equation, 36 bunched particle beams, 345, 349 dynamical Takatsuji model, 147 Fermi and Bose systems, 282 energy phase space, 292 Gaussian entropy model, 278 Maier–Saupe model, 198 multistable variability model, 341 negative stochastic feedback model, 356 noise generator, 350 numerics, 39 Plastino–Plastino model, 257 self-consistent, 38 two-layered, 36 Vlasov–Fokker–Planck equation, 344 Langevin force, 2, 37 Linear nonequilibrium thermodynamics, 80 Liquid crystals, 195 Lyapunov functionals, 78, 112 δ 2 S, 215

Index derivation of local Lyapunov functionals, 312 derivation of Lyapunov functionals, 317 free energy case, 78 Plastino–Plastino model, 255 stability analysis, 112 Master equation, 28, 369 Maximum entropy principle, 76 Mean field theory, 2 Metal electron model, 292 Mobility coefficient, 83 Moving frame transformations, 306 Multistability, 25 bounded B(M1 )-model, 152 Desai–Zwanzig model, 148 dynamical Takatsuji model, 140 KSS model, 157 Maier–Saupe model, 195 mean field HKB model, 167 multistable variability, 332 perception-action systems, 209 strongly nonlinear case, 43 symmetries, 186 Muscular contraction, 202 Noise noise amplitude, 1 noise generator, 349 noise source, 1 Nonlinear Fokker–Planck equations classifications, 26 entropy case, 213 Fermi and Bose systems energy phase space, 290 free energy case, 73 Landau form, 341 strongly nonlinear case, 31 Vlasov type, 343 with Boltzmann statistics, 109 Nonlinearity dimension, 25 Norm for perturbations, 132 Numerics Fokker–Planck equations, 28 Langevin equations, 39 Order parameters, 4

403

Parabolic partial differential equations, 365 Path integral solutions, 28 Planck’s radiation formula, 294 Plasma physics, 341 Polytropic gas, 248 Population dynamics, 296 Porous medium equation, 246 Propagation of molecular chaos, 55 Reentrant phase transitions, 329 Relativity theory, 296 Rhythmic single limb movements, 210 Self-consistency equations, 24 K-model, 121 KA -model, 124 bounded B(M1 ) model, 152 bounded B(A)-model, 125 compensated B(A)-model, 123 Desai–Zwanzig model, 149 dynamical Takatsuji model, 143 KSS model with sine coupling, 161 Maier–Saupe model, 198 mean field HKB model, 169 symmetric case, 170, 173 multistable variability model, 333 reentrant phase transitions, 330 Shimizu–Yamada model, 139 stability analysis, 115 Self-organization, 3 Smoluchowski limit, 284, 323 Stability analysis, 110 K-model, 120 KA -model, 124 bounded B(A)-model, 125 bounded B(M1 )-model, 153 compensated B(A)-model, 122 Desai–Zwanzig model, 149 dynamical Takatsuji model, 144 KSS model, 159, 163 linear stability analysis free energy case, 113 nonoscillatory instabilities, 299 Lyapunov’s direct method, 112 Maier–Saupe model, 198 mean field HKB model, 169 multiplicative noise, 130 multistable variability model, 333

404

Index

self-consistency equations, 115 Shiino’s decomposition of perturbations, 118 Shimizu–Yamada model, 139 Stationary solutions, 23 K-model, 121 KA -model, 124 bounded B(A)-model, 125 bounded B(M1 ) model, 152 compensated B(A)-model, 123 Desai–Zwanzig model, 149 dynamical Takatsuji model, 143 entropy case, 214 existence of stationary solutions, 153, 215 Fermi and Bose systems, 281 energy phase spaces, 290 free energy case, 75 with Boltzmann statistics, 109 KSS model free energy case, 158 with sine coupling, 161 linear nonequilibrium thermodynamics, 88 Maier–Saupe model, 198 mean field HKB model, 169 symmetric case, 170 negative stochastic feedback model, 353 Plastino–Plastino model, 251 reentrant phase transitions, 330 Sharma–Mittal model, 263 Shimizu–Yamada model, 135 strongly nonlinear case, 42 uniqueness of stationary solutions, 215 Stochastic feedback, 5, 34 Stochastic processes, 19 ensemble averaging, 19

hierarchy of distributions, 19 Markov diffusion processes, 2, 33 Ornstein–Uhlenbeck processes, 62 purely random processes, 61 statistical ensemble, 19 stochastic trajectory, 19 Wiener processes, 62 Stratonovich Fokker-Planck equation, 21 Langevin equation, 86 Superstatistics, 14 Synchronization, 191 applause, 191 brain activity, 193 planar rotators and phase oscillators, 194 tree crickets and fireflies, 192 Temperature fluctuations, 14 Thermodynamic flux, 81 Thermodynamic force, 81 Transient solutions, 22 Barenblatt–Pattle solutions, 249 Gaussian entropy model, 277 Gaussians, 63 Plastino–Plastino model, 253 Sharma–Mittal model, 268 Shimizu–Yamada model, 66 strongly nonlinear case, 55 Transition probability densities Gaussian entropy model, 276 Gaussians, 57 linear nonequilibrium thermodynamics, 86 Ornstein–Uhlenbeck processes, 62 Shimizu–Yamada model, 66 strongly nonlinear case, 55 Wiener processes, 62 Traveling waves, 324

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